KPL/FK Frame (FK) SPICE kernel file for JUICE-specific generic frames ============================================================================== This frames kernel defines a number of generic frames used by JUICE mission for Science opportunities identification, data analysis and scientific research. These frames are currently not ``built'' into the SPICE toolkit. These frames are sorted in two groups: those that are JUICE mission specific and those that are Jupiter system generic. The first group contains the frames defined by and for the JUICE mission, while the second provides the frames that are commonly accepted by the scientific community for the Jupiter system and its satellites. The IAU body-fixed rotational frames for Jupiter, Callisto, Europa and Ganymede is an exception to this grouping, as they are provided in a separate PCK kernel file. Version and Date ------------------------------------------------------------------------------ Version 1.3 -- November 30, 2022 -- Marc Costa Sitja, ESAC/ESA Alfredo Escalante Lopez, ESAC/ESA Renamed JUICE_JUP_THE_EXT_RING to JUICE_JUP_THE_RING_EXT. Updated ring reference frame base from from IAU_JUPITER to JUICE_JUPITER_IF_J2000. Added OBJECT_*_FRAME field for Plasma Tori and Jupiter Rings reference frames. Version 1.2 -- November 9, 2022 -- Ricardo Valles Blanco, ESAC/ESA Alfredo Escalante Lopez, ESAC/ESA Marc Costa Sitja, ESAC/ESA Renamed some Jupiter rings reference frames and included JUICE_JUP_THE_EXT_RING and JUICE_JUP_RING_BOUNDARY definitions. Added OBJECT__FRAME key to all frames to provide the body they are associated with (for usage with CIDFRM). Enhanced Jupiter Minor Moon descriptions with group classification. Version 1.1 -- July 21, 2022 -- Marc Costa Sitja, ESAC/ESA Alfredo Escalante Lopez, ESAC/ESA Tilmann Denk, DLR Added Jupiter satellites -- galilean moons, inner moons, and irregular moons -- names and abbreviations from Tilmann Denk and Jupiter rings and tori body/ID associations. Corrected typo in JUICE_GANYMEDE_MAG section name. Version 1.0 -- January 19, 2021 -- Alfredo Escalante Lopez, ESAC/ESA Added JUICE_JUP_HALO_RING, JUICE_JUP_MAIN_RING, JUICE_JUP_AMALTHEA_RING and JUICE_JUP_THEBE_RING reference frames. Version 0.9 -- November 16, 2021 -- Alfredo Escalante Lopez, ESAC/ESA Corrected JUICE_GANYMEDE_IF_J2000 class ID. Added JUICE_EPT Europa Plasma Torus reference frame. Version 0.8 -- September 22, 2020 -- Marc Costa Sitja, ESAC/ESA Elias Roussos, MPS Added the Ganymede Inertial Frame at J2000 (JUICE_GANYMEDE_IF_J2000) and Ganymede Magnetic reference frame (JUICE_GANYMEDE_MAG). Updated center of JUICE_IPT. Version 0.7 -- October 16, 2018 -- Marc Costa Sitja, ESAC/ESA Elias Roussos, MPS Validated and added a remark on the definition of JUICE_IPT frame. Version 0.6 -- October 10, 2018 -- Marc Costa Sitja, ESAC/ESA Renamed JUICE_JSEQ to JUICE_JSS to align it with the equivalent definition for the JUNO Frames Kernel. Duplicated JUPITER_SUN_ORB with JUICE_JSO and JUICE_SUN_EQU with JUICE_JH to align it with the equivalent definition for the JUNO Frames Kernel. Added first draft of JUICE Ion Plasma Torus frame. Version 0.5 -- August 16, 2016 -- Marc Costa Sitja, ESAC/ESA Jorge Diaz del Rio, ODC Space Renamed JUICE_JUPITER_BEQXS to JUICE_JSEQ. Updated the definition of JUICE_JUPITER_SIII_RH to be type-2, using data from 2009 IAU report and renamed frame to JUPITER_SYSTEM3RH_2009. Updated the definition of JUICE_JUPITER_MAG_SIII and renamed to JUPITER_MAG_VIP4. Added JUPITER_SYSTEM3RH_1965 using data from 1988-1994 IAU report. Added JUICE_JUPITER_MAG_S3RH2009, JUICE_JUPITER_MAGS_3RH1965 and JUICE_JUPITER_RTP frames. Added information about 'relative to' frames in section ``SPICE Frame names and NAIF ID Codes.'' Updated comments, frame descriptions and references. Version 0.4 -- July 21, 2016 -- Marc Costa Sitja, ESAC/ESA Updated the Jupiter generic frame definitions and format. Corrected errors in the JUICE_JUPITER_IF_J2000 and JUICE_JUPITER_DM definitions. Version 0.3 -- July 08, 2016 -- Marc Costa Sitja, ESAC/ESA The updates of this version have been motivated by the feedback of the JUICE Working Group 3 of the Science Operations Working Group iterated with NAIF. Updated reference [14] and added references [15], [16] and [17]. Added JUICE_JUPITER_IF_J2000 frame as described in reference [15] and as provided by Boris Semenov. Added a transformed version of CALLISTO_JUPITER_ORB, EUROPA_JUPITER_ORB and GANYMEDE_JUPITER_ORB frames to use the same convention as the community that models the local moon-magnetosphere interaction. The transformation applied is x'=-y, y'=x, z'=z. The new frames are JUICE_CALLISTO_PHI_ORB, JUICE_EUROPA_PHI_ORB and JUICE_GANYMEDE_PHI_ORB. Updated JUICE_JUPITER_MAG frame with dipole and prime meridians definitions from reference [16] as used by the JUNO mission. Changed name to JUICE_JUPITER_MAG_SIII. Added JUICE_JUPITER_SIII_RH frame as described in references [14] and [17]. Version 0.2 -- June 04, 2016 -- Marc Costa Sitja, ESAC/ESA Updated all NAIF ID codes from -907* to -28* since the JUICE spacecraft NAIF ID has been updated from -907 to -28. Added comments for future updates. Version 0.1 -- April 26, 2016 -- Jorge Diaz del Rio, ODC Space Modified frames' names to make them mission specific by adding JUICE_* Changed secondary axis in Jupiter Magnetic frame to be X instead of Y. Minor edits to comments and section descriptions. Version 0.0 -- February 5, 2016 -- Jorge Diaz del Rio, ODC Space Initial version. References ------------------------------------------------------------------------------ [1] "Frames Required Reading" [2] "Kernel Pool Required Reading" [3] Kivelson, M., Russell, C., 1995. "Introduction to Space Physics." Cambridge Univ. Press, Cambridge,UK. [4] http://stereo.sr.unh.edu/data/PLASTIC_Resources/ stereo_coordinates.pdf [5] Weiduo Hu, "Fundamental Spacecraft Dynamics and Control," Wiley 2015 [6] Bentley, R.D., Hapgood, M. and Thompson, W.T., "Coordinate Systems," 22-Mar-2010, HELIO-UCL=N3-003-TN. http://www.helio-vo.eu/documents/public/ HELIO_Coordinates_100322.pdf [7] Franz and Harper. (2002) "Heliospheric Coordinate Systems," Space Science, 50, 217ff. [8] Burlaga, L. F., 1984. "MHD processes in the outer heliosphere." Space Sci. Rev. 39, 255-316. [9] "Space Station Reference Coordinate Systems," Revision F, 26-Oct-2001 [10] Li, H., "Geostationary Satellites Collocation," Springer, 2014 [11] Russell, C.T., "Geophysical Coordinate Transformations," Cosmic Electrodynamics, 2, 184-196, 1971 [12] Bhavnani, K.H. and Vancour, R.P. (1991), "Coordinate Systems for Space and Geophysical Applications" [13] NASA/Marshall Solar Physics: http://solarscience.msfc.nasa.gov/SolarWind.shtml [14] Seidelmann, P.K., Divine, N. "Evaluation of Jupiter longitudes in System III (1965)", Geophysical Research Letters, Volume 4, Issue 2, Pages 65-68, 1977 [15] Liu X., Sachse, M., Spahn, F., Schmidt J., "Dynamics and distribution of Jovian dust ejected from the Galilean satellites", doi: 10.1002/2016JE004999, American Geophysical Union, 2016 [16] Connerney, J.E.P., Acuna, M.H., Ness N.F., Satoh, T., "New models of Jupiter's magnetic field constrained by the Io flux tube footprint", Journal of Geophysical Research, Vol. 103, No. A6, 929-939, 1998 [17] Bagenal F., Wilson, R.J., "Jupiter Coordinate Systems", ASP - U of Colorado, 07/15/16 http://lasp.colorado.edu/home/mop/missions/juno/coordinates/, accessed 21/07/16. [18] "Report of the IAU/IAG/COSPAR Working Group on Cartographic Coordinates and Rotational Elements of the Planets and Satellites: 1994." [19] Archinal, B.A., A'Hearn, M.F., Bowell, E., Conrad, A., Consolmagno, G.J., Courtin, R., Fukushima, T., Hestroffer, D., Hilton, J.L., Krasinsky, G.A., Neumann, G., Oberst, J., Seidelmann, P.K., Stooke, P., Tholen, D.J., Thomas, P.C., and Williams, I.P. "Report of the IAU Working Group on Cartographic Coordinates and Rotational Elements: 2009." [20] Dessler, A. J., "Appendix B: Coordinate Systems," in Physics of the Jovian Magnetosphere, Cambridge Univ. Press, A. J. Dessler, Ed., 1983. [21] JMAG Coordinate Systems, version 2. [22] JUNO Frames Kernel, version 12. https://naif.jpl.nasa.gov/pub/naif/JUNO/kernels/fk/juno_v12.tf [23] ''The configuration of Jupiter's magnetosphere'', Khurana, Krishan K. et al., Jupiter. The planet, satellites and magnetosphere. Cambridge planetary science, Vol. 1, Cambridge, UK, 2004 [24] ''Configuration of the Jovian magnetosphere'', Hill, T. W., Dessler, A. J. and Michel, F. C., Geophys. Res. Lett., 1974, doi:10.1029/GL001i001p00003 [25] Kivelson et al., ``The Permanent and Inductive Magnetic Moments of Ganymede'', Icarus 157, 507–522, 2002, doi:10.1006/icar.2002.6834 [26] Denk T., ``Outer Moons of Jupiter'', https://tilmanndenk.de/outerjovianmoons/ Accessed on November 4, 2022 Contact Information ------------------------------------------------------------------------------ If you have any questions regarding this file contact the ESA SPICE Service (ESS) at ESAC: Alfredo Escalante Lopez (+34) 91-8131-429 spice@sciops.esa.int or the JUICE Science Operations Center at ESAC: Marc Costa Sitja (+34) 646-746-711 Marc.Costa@ext.esa.int Implementation Notes ------------------------------------------------------------------------------ This file is used by the SPICE system as follows: programs that make use of this frame kernel must "load" the kernel normally during program initialization. Loading the kernel associates the data items with their names in a data structure called the "kernel pool". The routine that loads a kernel into the pool is shown below: FORTRAN: (SPICELIB) CALL FURNSH ( frame_kernel_name ) C: (CSPICE) furnsh_c ( frame_kernel_name ); IDL: (ICY) cspice_furnsh, frame_kernel_name MATLAB: (MICE) cspice_furnsh ( 'frame_kernel_name' ) This file was created and may be updated with a text editor or word processor JUICE Mission Natural Bodies and Science ID Codes ----------------------------------------------------------------------------- The following names and NAIF ID codes are assigned to the natural bodies and other science ``entities'' (the keywords implementing these definitions are located in the section "JUICE Mission NAIF ID Codes -- Definition Section" at the end of this file): JUICE Plasma Tori and Rings: Name ID Synonyms ------------------------- ------ -------------------------- JUICE_IO_PLASMA_TORUS -28968 JUICE_EUROPA_PLASMA_TORUS -28988 JUICE_JUP_RING_BOUNDARY -28941 JUICE_JUP_HALO_RING -28941 JUICE_JUP_MAIN_RING -28942 JUICE_JUP_AMA_GOS_RING -28943 JUICE_JUP_THE_GOS_RING -28944 JUICE_JUP_THE_RING_EXT -28945 JUICE Satellites with official NAIF ID codes and names: Name ID Synonyms --------------------- ------- -------------------------- IO 501 IO EUROPA 502 EU, EUR GANYMEDE 503 GA, GAN CALLISTO 504 CA, CAL AMALTHEA 505 AMA HIMALIA 506 HIM ELARA 507 ELA PASIPHAE 508 PAS SINOPE 509 SIN LYSITHEA 510 LYS CARME 511 CAR ANANKE 512 ANA LEDA 513 LED THEBE 514 THE ADRASTEA 515 ADR METIS 516 MET CALLIRRHOE 517 CLH THEMISTO 518 THM MEGACLITE 519 MEG TAYGETE 520 TAY CHALDENE 521 CHA HARPALYKE 522 HAR KALYKE 523 KLK IOCASTE 524 IOC ERINOME 525 ERI ISONOE 526 ISO PRAXIDIKE 527 PRA AUTONOE 528 AUT THYONE 529 THY HERMIPPE 530 HER AITNE 531 AIT EURYDOME 532 EYD EUANTHE 533 EUA EUPORIE 534 EUP ORTHOSIE 535 ORT SPONDE 536 SPO KALE 537 KLE PASITHEE 538 PST HEGEMONE 539 HEG MNEME 540 MNE AOEDE 541 AOE THELXINOE 542 TLX ARCHE 543 ARC KALLICHORE 544 KCH HELIKE 545 HLK CARPO 546 CRP EUKELADE 547 EUK CYLLENE 548 CYL KORE 549 KOR HERSE 550 HRS DIA 553 DIA JUICE Satellites without official names: Name ID Synonyms --------------------- ------- -------------------------- S2010_J1 551 S/2010_J_1, 10J1 S2010_J2 552 S/2010_J_2, 10J2 S2016_J1 554 S/2016_J_1, 16J1 S2003_J18 555 S/2003_J_18, 3J18 S2011_J 556 S/2011_J_2, 11J2 EIRENE 557 EIR PHILOPHROSYNE 558 PHI S2017_J1 559 S/2017_J_1, 17J1 EUPHEME 560 EPH S2003_J19 561 S/2003_J_19, 3J19 VALETUDO 562 VAL S2017_J2 563 S/2017_J_2, 17J2 S2017_J3 564 S/2017_J_3, 17J3 PANDIA 565 PDI S2017_J5 566 S/2017_J_5, 17J5 S2017_J6 567 S/2017_J_6, 17J6 S2017_J7 568 S/2017_J_7, 17J7 S2017_J8 569 S/2017_J_8, 17J8 S2017_J9 570 S/2017_J_9, 17J9 ERSA 571 ERS S2011_J1 572 S/2011_J_1, 11J1 S2003_J2 55501 S/2003_J_2, 3J2 S2003_J4 55502 S/2003_J_4, 3J4 S2003_J9 55503 S/2003_J_9, 3J9 S2003_J10 55504 S/2003_J_10, 3J10 S2003_J12 55505 S/2003_J_12, 3J12 S2003_J16 55506 S/2003_J_16, 3J16 S2003_J23 55507 S/2003_J_23, 3J23 S2003_J24 55508 S/2003_J_24, 3J24 JUICE Satellites classified by groups from [26] (duplicated from above): Group Name ID Synonyms ----------- --------------------- ------- -------------------------- Galilean IO 501 IO Galilean EUROPA 502 EU, EUR Galilean GANYMEDE 503 GA, GAN Galilean CALLISTO 504 CA, CAL Inner AMALTHEA 505 AMA Inner THEBE 514 THE Inner ADRASTEA 515 ADR Inner METIS 516 MET Ananke ANANKE 512 ANA Ananke HARPALYKE 522 HAR Ananke IOCASTE 524 IOC Ananke PRAXIDIKE 527 PRA Ananke THYONE 529 THY Ananke HERMIPPE 530 HER Ananke EUANTHE 533 EUA Ananke EUPORIE 534 EUP Ananke ORTHOSIE 535 ORT Ananke MNEME 540 MNE Ananke THELXINOE 542 TLX Ananke HELIKE 545 HLK Ananke S2010_J2 552 S/2010_J_2, 10J2 Ananke S2016_J1 554 S/2016_J_1, 16J1 Ananke S2003_J18 555 S/2003_J_18, 3J18 Ananke EUPHEME 560 EPH Ananke S2017_J3 564 S/2017_J_3, 17J3 Ananke S2017_J7 568 S/2017_J_7, 17J7 Ananke S2017_J9 570 S/2017_J_9, 17J9 Ananke S2003_J2 55501 S/2003_J_2, 3J2 Ananke S2003_J4 55502 S/2003_J_4, 3J4 Ananke S2003_J12 55505 S/2003_J_12, 3J12 Ananke S2003_J16 55506 S/2003_J_16, 3J16 Carme CARME 511 CAR Carme TAYGETE 520 TAY Carme CHALDENE 521 CHA Carme KALYKE 523 KLK Carme ERINOME 525 ERI Carme ISONOE 526 ISO Carme AITNE 531 AIT Carme KALE 537 KLE Carme PASITHEE 538 PST Carme ARCHE 543 ARC Carme KALLICHORE 544 KCH Carme EUKELADE 547 EUK Carme HERSE 550 HRS Carme S2010_J1 551 S/2010_J_1, 10J1 Carme EIRENE 557 EIR Carme S2003_J19 561 S/2003_J_19, 3J19 Carme S2017_J2 563 S/2017_J_2, 17J2 Carme S2017_J5 566 S/2017_J_5, 17J5 Carme S2017_J8 569 S/2017_J_8, 17J8 Carme S2011_J1 572 11_J_1, 11J1 Carme S2003_J9 55503 S/2003_J_9, 3J9 Carme S2003_J10 55504 S/2003_J_10, 3J10 Carme S2003_J24 55508 S/2003_J_24, 3J24 (*) Pasiphae PASIPHAE 508 PAS Pasiphae SINOPE 509 SIN Pasiphae CALLIRRHOE 517 CLH Pasiphae MEGACLITE 519 MEG Pasiphae AUTONOE 528 AUT Pasiphae EURYDOME 532 EYD Pasiphae SPONDE 536 SPO Pasiphae HEGEMONE 539 HEG Pasiphae AOEDE 541 AOE Pasiphae CYLLENE 548 CYL Pasiphae KORE 549 KOR Pasiphae S2011_J2 556 S/2011_J_2, 11J2 Pasiphae PHILOPHROSYNE 558 PHI Pasiphae S2017_J1 559 S/2017_J_1, 17J1 Pasiphae S2017_J6 567 S/2017_J_6, 17J6 Pasiphae S2003_J23 55507 S/2003_J_23, 3J23 Prograde (Thm) THEMISTO 518 THM Prograde (Him) HIMALIA 506 HIM Prograde (Him) ELARA 507 ELA Prograde (Him) LYSITHEA 510 LYS Prograde (Him) LEDA 513 LED Prograde (Him) DIA 553 DIA Prograde (Him) PANDIA 565 PDI Prograde (Him) ERSA 571 ERS Prograde (Crp) CARPO 546 CRP Prograde (Val) VALETUDO 562 VAL (*) Moon S/2003_J_24 from the Carme is not present in [26] but classified in: https://en.wikipedia.org/wiki/Moons_of_Jupiter (accessed Nov. 4, 2022). SPICE Frame names and NAIF ID Codes ------------------------------------------------------------------------------ The following generic frames are defined in this kernel file: SPICE Frame Name Long-name -------------------------- ------------------------------------------ JUICE mission specific generic frames(*): JUICE_JUPITER_IF_J2000 Jupiter Inertial Frame at J2000 JUICE_JUPITER_MAG_S3RH1965 Jupiter Magnetic System III VIP4 model using IAU 1994 constants JUICE_JUPITER_MAG_S3RH2009 Jupiter Magnetic System III VIP4 model using IAU 2009 constants JUICE_JSS Jovian-centric Equatorial Solar or Jupiter-De-Spun-Sun [22] JUICE_JUPITER_BSM Jupiter Solar Magnetospheric JUICE_JUPITER_SJC Solar Joviancentric Coordinates JUICE_JSM Jupiter Solar Magnetic JUICE_JSW Jupiter Solar Wind JUICE_JSWM Jupiter Solar Wind Magnetospheric JUICE_JSO Jupiter Solar Orbital (duplicate of JUPITER_SUN_ORB) JUICE_JH Jupiter Heliospheric (duplicate of JUPITER_SUN_EQU) JUICE_IPT Jupiter Io Plasma Torus JUICE_EPT Jupiter Europa Plasma Torus JUICE_CALLISTO_PHI_ORB Callisto-centered Phi-Zorb JUICE_EUROPA_PHI_ORB Europa-centered Phi-Zorb JUICE_GANYMEDE_PHI_ORB Ganymede-centered Phi-Zorb JUICE_GANYMEDE_IF_J2000 Ganymede Inertial Frame at J2000 JUICE_GANYMEDE_MAG Ganymede Magnetic Frame JUICE_HGRTN JUICE Heliocentric Radial-Tangential-Normal JUICE_SUN_RTN Sun-orbit JUICE Radial-Tangential-Normal JUICE_SUN_EQU_RTN Solar Equatorial Radial-Tangential-Normal JUICE_JUPITER_DM Jupiter JUICE Dipole Meridian JUICE_JUPITER_RTP JUICE Jupiter R-Theta-Phi JUICE_JUP_RING_BOUNDARY Jupiter Halo Ring Boundary Frame JUICE_JUP_HALO_RING Jupiter Halo Ring Frame JUICE_JUP_MAIN_RING Jupiter Main Ring Frame JUICE_JUP_AMA_GOS_RING Jupiter Amalthea Gossamer Ring Frame JUICE_JUP_THE_GOS_RING Jupiter Thebe Gossamer Ring Frame JUICE_JUP_THE_RING_EXT Jupiter Thebe Gossamer Ring Frame Jupiter system generic frames(**): JUPITER_SYSTEM3RH_1965 Jupiter System III Right-handed using the IAU 1994 constants JUPITER_SYSTEM3RH_2009 Jupiter System III Right-handed using the IAU 2009 constants JUPITER_MAG_VIP4 Jupiter Magnetic System III VIP4 JUPITER_MEQUD Jupiter Mean Equator of date JUPITER_SUN_EQU Jupiter Solar Equatorial JUPITER_SUN_ORB Jupiter Solar Orbital JUPITER_CALLISTO_BCSF Jupiter-centric Callisto-following JUPITER_EUROPA_BCSF Jupiter-centric Europa-following JUPITER_GANYMEDE_BCSF Jupiter-centric Ganymede-following CALLISTO_JUPITER_ORB Callisto Orbital EUROPA_JUPITER_ORB Europa Orbital GANYMEDE_JUPITER_ORB Ganymede Orbital (*) The definition of the dipole direction of these frames needs to be discussed within the Science Operations Working Team Working Group 3 in coordination with Juno and Europa Multi Fly-by Mission. The name for JUICE_SUN_RTN also needs to be discussed. (**) These frames are commonly used by other missions for data analysis and scientific research. In the future NAIF may include them in their official generic frames kernel for the Jupiter system. When this happens the frames will be removed from this kernel. These frames have the following centers, frame class and NAIF IDs: SPICE Frame Name Center Class NAIF ID -------------------------- ---------------------- ------- --------- JUICE_JUPITER_IF_J2000 JUPITER FIXED -28970 JUICE_JUPITER_MAG_S3RH1965 JUPITER FIXED -28971 JUICE_JUPITER_MAG_S3RH2009 JUPITER FIXED -28972 JUICE_JSS JUPITER DYNAMIC -28973 JUICE_JUPITER_BSM JUPITER DYNAMIC -28974 JUICE_JUPITER_SJC JUPITER DYNAMIC -28975 JUICE_JSM JUPITER DYNAMIC -28976 JUICE_JSW JUPITER FIXED -28977 JUICE_JSWM JUPITER FIXED -28978 JUICE_JSO JUPITER DYNAMIC -28979 JUICE_JH JUPITER DYNAMIC -28969 JUICE_IPT JUICE_IO_PLASMA_TORUS DYNAMIC -28968 JUICE_EPT JUICE_EUROPA_PLASMA_TORUS DYNAMIC -28988 JUICE_CALLISTO_PHI_ORB CALLISTO DYNAMIC -28980 JUICE_EUROPA_PHI_ORB EUROPA DYNAMIC -28981 JUICE_GANYMEDE_PHI_ORB GANYMEDE DYNAMIC -28982 JUICE_GANYMEDE_IF_J2000 GANYMEDE FIXED -28983 JUICE_GANYMEDE_MAG GANYMEDE FIXED -28984 JUICE_HGRTN SUN DYNAMIC -28990 JUICE_SUN_RTN JUICE DYNAMIC -28991 JUICE_SUN_EQU_RTN JUICE DYNAMIC -28994 JUICE_JUPITER_DM JUPITER DYNAMIC -28992 JUICE_JUPITER_RTP JUPITER DYNAMIC -28993 JUICE_JUP_RING_BOUNDARY JUPITER FIXED -28940 JUICE_JUP_HALO_RING JUICE_JUP_HALO_RING FIXED -28941 JUICE_JUP_MAIN_RING JUICE_JUP_MAIN_RING FIXED -28942 JUICE_JUP_AMA_GOS_RING JUICE_JUP_AMA_GOS_RING FIXED -28943 JUICE_JUP_THE_GOS_RING JUICE_JUP_THE_GOS_RING FIXED -28944 JUICE_JUP_THE_RING_EXT JUICE_JUP_THE_RING_EXT FIXED -28945 JUPITER_SYSTEM3RH_1965 JUPITER PCK -28999 JUPITER_SYSTEM3RH_2009 JUPITER PCK -28998 JUPITER_MAG_VIP4 JUPITER FIXED -28997 JUPITER_MEQUD JUPITER DYNAMIC 500599000 JUPITER_SUN_EQU JUPITER DYNAMIC 500599001 JUPITER_SUN_ORB JUPITER DYNAMIC 500599002 JUPITER_CALLISTO_BCSF JUPITER DYNAMIC 500599006 JUPITER_EUROPA_BCSF JUPITER DYNAMIC 500599004 JUPITER_GANYMEDE_BCSF JUPITER DYNAMIC 500599005 CALLISTO_JUPITER_ORB CALLISTO DYNAMIC 500504000 EUROPA_JUPITER_ORB EUROPA DYNAMIC 500502000 GANYMEDE_JUPITER_ORB GANYMEDE DYNAMIC 500503000 These frames have been defined relative to the following frames: SPICE Frame Name Relative to -------------------------- ---------------------- JUICE_JUPITER_IF_J2000 J2000 JUICE_JUPITER_MAG_S3RH1965 JUPITER_SYSTEM3RH_1965 JUICE_JUPITER_MAG_S3RH2009 JUPITER_SYSTEM3RH_2009 JUICE_JSS J2000 JUICE_JUPITER_BSM J2000 JUICE_JUPITER_SJC J2000 JUICE_JSM J2000 JUICE_JSW JUPITER_SUN_ORB (1) JUICE_JSWM JUICE_JUPITER_BSM (1) JUICE_JSO J2000 JUICE_JH J2000 JUICE_IPT JUPITER_SYSTEM3RH_2009 JUICE_EPT J2000 JUICE_CALLISTO_PHI_ORB J2000 JUICE_EUROPA_PHI_ORB J2000 JUICE_GANYMEDE_PHI_ORB J2000 JUICE_GANYMEDE_IF_J2000 J2000 JUICE_GANYMEDE_MAG IAU_GANYMEDE JUICE_HGRTN J2000 JUICE_SUN_RTN J2000 JUICE_SUN_EQU_RTN J2000 JUICE_JUPITER_DM J2000 JUICE_JUPITER_RTP J2000 JUICE_JUP_RING_BOUNDARY JUICE_JUPITER_IF_J2000 JUICE_JUP_HALO_RING JUICE_JUPITER_IF_J2000 JUICE_JUP_MAIN_RING JUICE_JUPITER_IF_J2000 JUICE_JUP_AMA_GOS_RING JUICE_JUPITER_IF_J2000 JUICE_JUP_THE_GOS_RING JUICE_JUPITER_IF_J2000 JUICE_JUP_THE_RING_EXT JUICE_JUPITER_IF_J2000 JUPITER_SYSTEM3RH_1965 J2000 JUPITER_SYSTEM3RH_2009 J2000 JUPITER_MAG_VIP4 IAU_JUPITER JUPITER_MEQUD J2000 JUPITER_SUN_EQU J2000 JUPITER_SUN_ORB J2000 JUPITER_CALLISTO_BCSF J2000 JUPITER_EUROPA_BCSF J2000 JUPITER_GANYMEDE_BCSF J2000 CALLISTO_JUPITER_ORB J2000 EUROPA_JUPITER_ORB J2000 GANYMEDE_JUPITER_ORB J2000 (1) SPICE imposes a constraint in the definition of dynamic frames (see [1]): When the definition of a parameterized dynamic frame F1 refers to a second frame F2 the referenced frame F2 may be dynamic, but F2 must not make reference to any dynamic frame. Therefore, no other dynamic frame should make reference to this frame. The keywords implementing these frame definitions are located in the "JUICE Mission Specific Generic Frame Definitions" and "JUPITER System Generic Frame Definitions" sections. General Notes About This File ------------------------------------------------------------------------------ About Required Data: -------------------- Most of the dynamic frames defined in this file require at least one of the following kernels to be loaded prior to their evaluation, normally during program initialization: - Planetary ephemeris data (SPK), e.g. DE403, DE405, etc; - Planetary constants data (PCK); - Earth generic frames definitions (FK). Note that loading different kernels will lead to different orientations of the same frame at a given epoch, providing different results from each other, in terms of state vectors referred to these frames. About Implementation: --------------------- The SPICE frames defined within this file and their corresponding references in literature might not be equivalent, both due to variations in the SPICE kernels on which the SPICE frame depends, and due to possible differences in both the frame's definition and implementation (e.g. GSE can be defined using the instantaneous orbital plane or mean ecliptic; the mean ecliptic is a function of the ecliptic model). Please refer to each applicable frame description section for particular details on the current SPICE kernel implementation. JUICE Mission Specific Scientific Frame Definitions ------------------------------------------------------------------------------ This section contains the definition of the JUICE mission specific scientific frames. Jupiter Inertial Frame at J2000 (JUICE_JUPITER_IF_J2000) ------------------------------------------------------------------------ Definition: ----------- The Jupiter Inertial Frame at J2000 is defined as follows: - +Z axis is parallel to Jupiter rotation axis at J2000, pointing toward the North side of the invariable plane; - +X axis is aligned with the ascending node of the Jovian orbital plane with the Jovian equator plane at J2000; - +Y axis completes the right-handed system; - the origin of this frame is the center of mass of Jupiter. All vectors are geometric: no aberration corrections are used. Remarks: -------- This frame is defined as a fixed offset frame using constant vectors as the specification method. The fixed offset for these vectors were based on the following directions (that also define a two-vector frame): - +Z axis along Right Ascension of 268.05720404270755 degrees and Declination of 64.495809953395721 of Jupiter pole at J2000 epoch in J2000 inertial frame; - +X axis along Right Ascension of 139.90957808624046 degrees and Declination of 16.419104754306645 with respect to J2000 inertial frame at J2000 epoch, which corresponds to the RA/DEC of Jupiter instantaneous orbital plane ascending node on Jupiter equator at J2000 epoch in J2000 inertial frame; This frame has been defined based on the IAU_JUPITER frame, whose evaluation was based on the data included in the loaded PCK file. When evaluated, the IAU 2009 constants for Jupiter (see [19]) were used. In addition jup310.bsp has been used to compute the Jupiter instantaneous orbital plane ascending node on Jupiter equator at J2000 epoch in J2000 inertial frame. \begindata FRAME_JUICE_JUPITER_IF_J2000 = -28970 FRAME_-28970_NAME = 'JUICE_JUPITER_IF_J2000' FRAME_-28970_CLASS = 4 FRAME_-28970_CLASS_ID = -28970 FRAME_-28970_CENTER = 599 TKFRAME_-28970_SPEC = 'ANGLES' TKFRAME_-28970_RELATIVE = 'J2000' TKFRAME_-28970_ANGLES = ( -88.057204042707568 25.504190046604286 -48.968728165793905 ) TKFRAME_-28970_AXES = ( 3, 2, 3 ) TKFRAME_-28970_UNITS = 'DEGREES' \begintext Jupiter Magnetic S3RH VIP4 model - IAU 1994 (JUICE_JUPITER_MAG_S3RH1965) ------------------------------------------------------------------------ SPICE frame name, common names and other designators: ----------------------------------------------------- Within the SPICE system, the Jupiter Magnetic System III Right-handed frame using the VIP4 model (see [16]) and IAU 1994 constants (see [18]) is referred as JUICE_JUPITER_MAG_S3RH1965. Definition: ----------- The Jupiter Magnetic System III Right-Handed frame is defined as follows (from [17]): - +Z axis is parallel to the magnetic dipole axis of epoch and aligned with the North magnetic pole of epoch; - +Y axis is defined with respect to the meridian where the magnetic and geographic equators cross at longitude 249.2 degrees in the System III Right-handed frame; - +X completes the right-handed frame; - the origin of this frame is the center of mass of Jupiter. Remarks: -------- This frame is base on the VIP4 model (see [16]) using as reference the System III Right-handed body-fixed frame for Jupiter with the constants provided in the IAU 1994 report (see [18]) for Jupiter's north pole and primer meridian location. The magnetic system rotates with Jupiter at the same rate, but about the magnetic dipole instead of the Jovian spin axis. The north dipole location is the best-fit, centered dipole magnetic moment vector M direction in the JUPITER_SYSTEM3RH_1965 frame based on the VIP4 model. M is defined to be titled 9.50 degrees away from the Jovian spin axis towards longitude 200.8 degrees West, therefore, the current values for the Jupiter north magnetic centered dipole planetocentric coordinates are: Longitude = 159.2 (degrees) Latitude = 80.5 (degrees) \begindata FRAME_JUICE_JUPITER_MAG_S3RH1965 = -28971 FRAME_-28971_NAME = 'JUICE_JUPITER_MAG_S3RH1965' FRAME_-28971_CLASS = 4 FRAME_-28971_CLASS_ID = -28971 FRAME_-28971_CENTER = 599 TKFRAME_-28971_SPEC = 'ANGLES' TKFRAME_-28971_RELATIVE = 'JUPITER_SYSTEM3RH_1965' TKFRAME_-28971_ANGLES = ( 0, -159.2, -9.5 ) TKFRAME_-28971_AXES = ( 2, 3, 2 ) TKFRAME_-28971_UNITS = 'DEGREES' \begintext Jupiter Magnetic S3RH VIP4 model - IAU 2009 (JUICE_JUPITER_MAG_S3RH2009) ------------------------------------------------------------------------ SPICE frame name, common names and other designators: ----------------------------------------------------- Within the SPICE system, the Jupiter Magnetic System III Right-handed frame using the VIP4 model and IAU 2009 constants is referred as JUICE_JUPITER_MAG_S3RH2009. Definition: ----------- The Jupiter Magnetic System III Right-Handed frame is defined as follows (from [17]): - +Z axis is parallel to the magnetic dipole axis of epoch and aligned with the North magnetic pole of epoch; - +Y axis is defined with respect to the meridian where the magnetic and geographic equators cross at longitude 249.2 degrees in the System III Right-handed frame; - +X completes the right-handed frame; - the origin of this frame is the center of mass of Jupiter. Remarks: -------- This frame is base on the VIP4 model (see [16]) using as reference the System III Right-handed body-fixed frame for Jupiter with the constants provided in the IAU 2009 report (see [19]) for Jupiter's north pole and primer meridian location. The magnetic system rotates with Jupiter at the same rate, but about the magnetic dipole instead of the Jovian spin axis. The north dipole location is the best-fit, centered dipole magnetic moment vector M direction in the JUPITER_SYSTEM3RH_2009 frame based on the VIP4 model. M is defined to be titled 9.50 degrees away from the Jovian spin axis towards longitude 200.8 degrees West, therefore, the current values for the Jupiter north magnetic centered dipole planetocentric coordinates are: Longitude = 159.2 (degrees) Latitude = 80.5 (degrees) \begindata FRAME_JUICE_JUPITER_MAG_S3RH2009 = -28972 FRAME_-28972_NAME = 'JUICE_JUPITER_MAG_S3RH2009' FRAME_-28972_CLASS = 4 FRAME_-28972_CLASS_ID = -28972 FRAME_-28972_CENTER = 599 TKFRAME_-28972_SPEC = 'ANGLES' TKFRAME_-28972_RELATIVE = 'JUPITER_SYSTEM3RH_2009' TKFRAME_-28972_ANGLES = ( 0, -159.2, -9.5 ) TKFRAME_-28972_AXES = ( 2, 3, 2 ) TKFRAME_-28972_UNITS = 'DEGREES' \begintext Joviancentric Equatorial Solar frame (JUICE_JSS) ------------------------------------------------------------------------ SPICE frame name, common names and other designators: ----------------------------------------------------- Within the SPICE system, and for the JUICE mission, the Joviancentric Equatorial Solar frame or Jupiter-De-Spun-Sun is referred as JUICE_JSS. In the documentation provided by the JUICE MAG team (see [21]), it is referred as Joviancentric Solar Equatorial frame or JSEq. Definition: ----------- The Joviancentric Equatorial Solar frame is defined as follows (from [4]): - X-Y plane is defined by the Jupiter equator of date. Therefore, the +Z axis is the primary vector and it is aligned to Jupiter's north pole of date; - +X axis is the component of the position of Jupiter relative to the Sun that is orthogonal to the +Z axis; - +Y axis completes the right-handed system; - the origin of this frame is the center of mass of Jupiter. All vectors are geometric: no aberration corrections are used. Uses and applications: ---------------------- The Joviancentric Equatorial Solar frame is commonly used in the analysis of orbital trajectories where planetary rotation complicates the analysis but where knowledge of the equatorial plane is still required. Data can be analyzed for local time and north-south asymmetries in this reference frame. Required Data: -------------- This frame is defined as a two-vector frame using two different types of specifications for the primary and secondary vectors. The primary vector is defined as a constant vector in the IAU_JUPITER body-fixed frame, which is a PCK-based frame. Therefore a PCK file containing the orientation constants for Jupiter must be loaded before using this frame. The secondary vector is defined as an 'observer-target position' vector. Therefore, the ephemeris data required to compute the Sun-Jupiter position vector in the J2000 reference frame must be loaded before using this frame. Remarks: -------- This frame is defined based on SPK data: different planetary ephemerides for Jupiter, Jupiter's Barycenter, the Sun and the Solar System Barycenter will lead to different frame orientation at a given time. This frame is also defined based on the IAU_JUPITER frame, whose evaluation is based on the data included in the loaded PCK file: different orientation constants for Jupiter's spin axis will lead to different frame orientation at a given time. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. JUICE_JSEQ using the IAU 2009 constants and the DE405 ephemeris. \begindata FRAME_JUICE_JSS = -28973 FRAME_-28973_NAME = 'JUICE_JSS' FRAME_-28973_CLASS = 5 FRAME_-28973_CLASS_ID = -28973 FRAME_-28973_CENTER = 599 FRAME_-28973_RELATIVE = 'J2000' FRAME_-28973_DEF_STYLE = 'PARAMETERIZED' FRAME_-28973_FAMILY = 'TWO-VECTOR' FRAME_-28973_PRI_AXIS = 'Z' FRAME_-28973_PRI_VECTOR_DEF = 'CONSTANT' FRAME_-28973_PRI_FRAME = 'IAU_JUPITER' FRAME_-28973_PRI_SPEC = 'RECTANGULAR' FRAME_-28973_PRI_VECTOR = ( 0, 0, 1 ) FRAME_-28973_SEC_AXIS = 'X' FRAME_-28973_SEC_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_-28973_SEC_OBSERVER = 'JUPITER' FRAME_-28973_SEC_TARGET = 'SUN' FRAME_-28973_SEC_ABCORR = 'NONE' \begintext Jupiter Solar Magnetospheric (JUICE_JUPITER_BSM) ------------------------------------------------------------------------ SPICE frame name, common names and other designators: ----------------------------------------------------- Within the SPICE system, the Jupiter Solar Magnetospheric frame is referred as JUICE_SUN_BSM. In the documentation provided by the JUICE MAG team (see [21]),, this frame is referred as JSM. Definition: ----------- The Jupiter Solar Magnetospheric frame is defined, based on the definition in [11] for the Earth, as follows (from [21]): - +X axis is the position of the Sun relative to Jupiter; it's the primary vector and points from Jupiter to the Sun; - +Z axis is the projection of the magnetic centered dipole axis (positive North) of Jupiter onto the plane perpendicular to the +X axis. - +Y axis completes the right-handed system; - the origin of this frame is the center of mass of Jupiter. All vectors are geometric: no aberration corrections are used. Uses and applications: ---------------------- The Jupiter Solar Magnetospheric is used to analyze data affected by both the solar wind flow velocity and the rotating magnetic field of Jupiter, but where the solar wind forces still dominate (in the magnetosheath and near the magnetopause) (from [21]). Required Data: -------------- This frame is defined as a two-vector frame using two different types of specifications for the primary and secondary vectors. The primary vector is defined as an 'observer-target position' vector. Therefore, the ephemeris data required to compute the Jupiter-Sun position vector in the J2000 reference frame must be loaded before using this frame. The secondary vector is defined as a constant vector in the JUPITER_MAG_VIP4 body-fixed frame, which provides the orientation for the Jupiter North magnetic dipole and the Jupiter magnetic frame with respect to the IAU_JUPITER body-fixed frame. Remarks: -------- This frame is defined based on SPK data: different planetary ephemerides for Jupiter, Jupiter Barycenter, the Sun and the Solar System Barycenter will lead to a different frame orientation at a given time. This frame is also defined based on the JUPITER_MAG_VIP4 frame, which is defined relative to the IAU_JUPITER frame, whose evaluation is based on the data included in the loaded PCK file: different orientation constants for Jupiter's spin axis will lead to different frame orientation at a given time, but only when these constants result on different projections of the north magnetic centered dipole on the frame's YZ plane. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. JUICE_JUPITER_BSM using the IAU 2009 constants and the DE405 ephemeris. \begindata FRAME_JUICE_JUPITER_BSM = -28974 FRAME_-28974_NAME = 'JUICE_JUPITER_BSM' FRAME_-28974_CLASS = 5 FRAME_-28974_CLASS_ID = -28974 FRAME_-28974_CENTER = 599 FRAME_-28974_RELATIVE = 'J2000' FRAME_-28974_DEF_STYLE = 'PARAMETERIZED' FRAME_-28974_FAMILY = 'TWO-VECTOR' FRAME_-28974_PRI_AXIS = 'X' FRAME_-28974_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_-28974_PRI_OBSERVER = 'JUPITER' FRAME_-28974_PRI_TARGET = 'SUN' FRAME_-28974_PRI_ABCORR = 'NONE' FRAME_-28974_SEC_AXIS = 'Z' FRAME_-28974_SEC_VECTOR_DEF = 'CONSTANT' FRAME_-28974_SEC_SPEC = 'RECTANGULAR' FRAME_-28974_SEC_VECTOR = ( 0, 0, 1 ) FRAME_-28974_SEC_FRAME = 'JUPITER_MAG_VIP4' \begintext Solar Joviancentric Coordinates frame (JUICE_JUPITER_SJC) ------------------------------------------------------------------------ SPICE frame name, common names and other designators: ----------------------------------------------------- Within the SPICE system, and for the JUICE mission, the Solar Joviancentric Coordinates frame is referred as JUICE_JUPITER_SJC. In the documentation provided by the JUICE MAG team (see [21]), it is referred as Solar Joviancentric Coordinates or SJ. Definition: ----------- The Solar Joviancentric Coordinates frame is defined as follows (from [21]): - +X axis is the position of the Sun relative to Jupiter; it's the primary vector and points from Jupiter to the Sun; - +Z axis is the component of Jupiter's north pole of date orthogonal to the +X axis; - +Y axis completes the right-handed reference frame; - the origin of this frame is the center of mass of Jupiter. All vectors are geometric: no aberration corrections are used. Required Data: -------------- This frame is defined as a two-vector frame using two different types of specifications for the primary and secondary vectors. The primary vector is defined as an 'observer-target position' vector. Therefore, the ephemeris data required to compute the Jupiter-Sun vector in the J2000 reference frame must be loaded before using this frame. The secondary vector is defined as a constant vector in the IAU_JUPITER body-fixed frame, which is a PCK-based frame. Therefore a PCK file containing the orientation constants for Jupiter must be loaded before using this frame. Remarks: -------- This frame is defined based on SPK data: different planetary ephemerides for Jupiter, Jupiter Barycenter, the Sun and the Solar System Barycenter will lead to a different frame orientation at a given time. This frame is also defined based on the IAU_JUPITER frame, whose evaluation is based on the data included in the loaded PCK file: different orientation constants for Jupiter's spin axis will lead to a different frame orientation at a given time. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. JUICE_JUPITER_SJC using the IAU 2009 constants and the DE405 ephemeris. \begindata FRAME_JUICE_JUPITER_SJC = -28975 FRAME_-28975_NAME = 'JUICE_JUPITER_SJC' FRAME_-28975_CLASS = 5 FRAME_-28975_CLASS_ID = -28975 FRAME_-28975_CENTER = 599 FRAME_-28975_RELATIVE = 'J2000' FRAME_-28975_DEF_STYLE = 'PARAMETERIZED' FRAME_-28975_FAMILY = 'TWO-VECTOR' FRAME_-28975_PRI_AXIS = 'X' FRAME_-28975_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_-28975_PRI_OBSERVER = 'JUPITER' FRAME_-28975_PRI_TARGET = 'SUN' FRAME_-28975_PRI_ABCORR = 'NONE' FRAME_-28975_SEC_AXIS = 'Z' FRAME_-28975_SEC_VECTOR_DEF = 'CONSTANT' FRAME_-28975_SEC_FRAME = 'IAU_JUPITER' FRAME_-28975_SEC_SPEC = 'RECTANGULAR' FRAME_-28975_SEC_VECTOR = ( 0, 0, 1 ) \begintext Jupiter Solar Magnetic (JUICE_JSM) ------------------------------------------------------------------------ Definition: ----------- The Jupiter Solar Magnetic frame is defined, based on the definition provided in [11] for the Earth's solar magnetic frame, as follows: - +Z axis is aligned with the North magnetic centered dipole of Jupiter; - +X axis is the component of the Jupiter-Sun vector that is orthogonal to the +Z axis; - +Y axis completes the right-handed system; - the origin of this frame is the center of mass of Jupiter. All vectors are geometric: no aberration corrections are used. Required Data: -------------- This frame is defined as a two-vector frame using two different types of specifications for the primary and secondary vectors. The primary vector is defined as a constant vector in the JUPITER_MAG_VIP4 body-fixed frame, which provides the orientation for the Jupiter North magnetic dipole and the Jupiter magnetic frame with respect to the IAU_JUPITER body-fixed frame. The secondary vector is defined as an 'observer-target position' vector. Therefore, the ephemeris data required to compute the Jupiter-Sun position vector in the J2000 reference frame must be loaded before using this frame. Remarks: -------- This frame is defined based on SPK data: different planetary ephemerides for Jupiter, Jupiter's Barycenter, the Sun and the Solar System Barycenter will lead to different frame orientation at a given time. This frame is also defined based on the JUPITER_MAG_VIP4 frame, which is defined relative to the IAU_JUPITER frame, whose evaluation is based on the data included in the loaded PCK file: different orientation constants for Jupiter's spin axis will lead to different frame orientation at a given time. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. JUICE_JSM using the IAU 2009 constants and the DE405 ephemeris. \begindata FRAME_JUICE_JSM = -28976 FRAME_-28976_NAME = 'JUICE_JSM' FRAME_-28976_CLASS = 5 FRAME_-28976_CLASS_ID = -28976 FRAME_-28976_CENTER = 599 FRAME_-28976_RELATIVE = 'J2000' FRAME_-28976_DEF_STYLE = 'PARAMETERIZED' FRAME_-28976_FAMILY = 'TWO-VECTOR' FRAME_-28976_PRI_AXIS = 'Z' FRAME_-28976_PRI_VECTOR_DEF = 'CONSTANT' FRAME_-28976_PRI_SPEC = 'RECTANGULAR' FRAME_-28976_PRI_VECTOR = ( 0, 0, 1 ) FRAME_-28976_PRI_FRAME = 'JUPITER_MAG_VIP4' FRAME_-28976_SEC_AXIS = 'X' FRAME_-28976_SEC_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_-28976_SEC_OBSERVER = 'JUPITER' FRAME_-28976_SEC_TARGET = 'SUN' FRAME_-28976_SEC_ABCORR = 'NONE' \begintext Jupiter Solar Wind frame (JUICE_JSW) ------------------------------------------------------------------------ Definition: ----------- The Jupiter Solar Wind frame is defined is defined, based on the definition in [12], section 3.3.7) for the Geocentric Solar Wind frame, as follows: - +Z is perpendicular to the orbital plane of Jupiter and is positive towards North; - +X axis is the component of the solar wind direction vector that is orthogonal to the +Z-axis. This axis lies in the orbital plane of Jupiter and is positive in the direction opposite to the solar wind; - +Y axis completes the right-handed system; - the origin of this frame is the center of mass of Jupiter. Uses and applications: ---------------------- The Jupiter Solar Wind frame is useful in analyzing the impact of solar wind on hemispheric events (from [12], section 3.3.7). Remarks: -------- A critical issue to consider in the definition of this frame is aberration - the bow shock of Jupiter is rotated in the plane of the orbit of Jupiter by angle Vplanet/Vsolar_wind, where Vplanet is the velocity of Jupiter in its orbit and Vsolar_wind is the solar wind speed. The sense of rotation is such the bow shock lags its un-rotated location on the anti-sunward side of Jupiter. This is the +Y direction for Jupiter solar orbital frame (JUPITER_SUN_ORB). Strictly speaking Vplanet should be the component perpendicular to the solar wind. Th solar wind streams off of the Sun in all directions at speeds of about 400 km/s. Nevertheless, the solar wind is not uniform. Although it is always directed away from the Sun, it changes speed and carries with it magnetic clouds, interacting regions where high speed wind catches up with slow speed wind, and composition variations. The solar wind speed can range from high (800 km/s) over coronal holes to low velocities (300 km/s) over streamers (see [13]). For Jupiter under normal solar wind conditions (v ~400 km/s) the angle of aberration ranges from 1.9652 degrees for the maximum orbital velocity to 1.7819 degrees for the minimum orbital velocity of Jupiter. By convention, the average velocity for Jupiter in its orbit and for the solar wind at Jupiter will be used in the definition of this frame, which is highly significant for determining magnetopause and bow shock locations. This value is determined to be 1.8707 degrees. Since the minimum aberration is of approximately 0.89095 degrees (maximum solar wind and minimum Jupiter orbital velocities) and the maximum aberration is of approximately 2.6203 degrees (minimum solar wind and maximum Jupiter orbital velocities), the error in the definition of the +X-axis direction is between -0.97975 to 0.7496 degrees. This frame is defined relative to JUPITER_SUN_ORB, which is dynamic. This aspect shall be taken into account if/when using this frame to define other dynamic frames. For further details, please refer to [1]. \begindata FRAME_JUICE_JSW = -28977 FRAME_-28977_NAME = 'JUICE_JSW' FRAME_-28977_CLASS = 4 FRAME_-28977_CLASS_ID = -28977 FRAME_-28977_CENTER = 599 TKFRAME_-28977_SPEC = 'ANGLES' TKFRAME_-28977_RELATIVE = 'JUPITER_SUN_ORB' TKFRAME_-28977_ANGLES = ( -1.8707, 0.0, 0.0 ) TKFRAME_-28977_AXES = ( 3, 2, 3 ) TKFRAME_-28977_UNITS = 'DEGREES' \begintext Jupiter Solar Wind Magnetospheric frame (JUICE_JSWM) ------------------------------------------------------------------------ Definition: ----------- The Jupiter solar wind magnetospheric frame is defined, based on the definition in [12], section 3.3.6) for the Geocentric Solar Wind Magnetospheric frame, as follows: - +X axis is aligned with the solar wind direction. This axis is positive in the direction opposite to the solar wind; - +Z axis is the component of the magnetic axis (magnetic dipole) orthogonal to the +X axis, positive towards magnetic north of Jupiter; - +Y axis completes the right-handed system. It is perpendicular to the magnetic axis (magnetic dipole); - the origin of this frame is the center of mass of Jupiter. All vectors are geometric: no aberration corrections are used. Remarks: -------- A critical issue to consider in the definition of this frame is aberration - the bow shock of Jupiter is rotated in the plane of the orbit of Jupiter by angle Vplanet/Vsolar_wind, where Vplanet is the velocity of Jupiter in its orbit and Vsolar_wind is the solar wind speed. The sense of rotation is such the bow shock lags its un-rotated location on the anti-sunward side of Jupiter. This is the +Y direction for Jupiter Solar Orbital frame (JUPITER_SUN_ORB). Strictly speaking Vplanet should be the component perpendicular to the solar wind. Th solar wind streams off of the Sun in all directions at speeds of about 400 km/s. Nevertheless, the solar wind is not uniform. Although it is always directed away from the Sun, it changes speed and carries with it magnetic clouds, interacting regions where high speed wind catches up with slow speed wind, and composition variations. The solar wind speed can range from high (800 km/s) over coronal holes to low velocities (300 km/s) over streamers (see [13]). For Jupiter under normal solar wind conditions (v ~400 km/s) the angle of aberration ranges from 1.9652 degrees for the maximum orbital velocity to 1.7819 degrees for the minimum orbital velocity of Jupiter. By convention, the average velocity for Jupiter in its orbit and for the solar wind at Jupiter, will be used in the definition of this frame, which is highly significant for determining magnetopause and bow shock locations. This value is determined to be 1.8707 degrees. Since the minimum aberration is of approximately 0.89095 degrees (maximum solar wind and minimum Jupiter orbital velocities) and the maximum aberration is of approximately 2.6203 degrees (minimum solar wind and maximum Jupiter orbital velocities), the error in the definition of the +X-axis direction is between -0.97975 to 0.7496 degrees. This frame is defined relative to JUICE_JUPITER_BSM, which is dynamic. This aspect shall be taken into account if/when using this frame to define other dynamic frames. For further details, please refer to [1]. \begindata FRAME_JUICE_JSWM = -28978 FRAME_-28978_NAME = 'JUICE_JSWM' FRAME_-28978_CLASS = 4 FRAME_-28978_CLASS_ID = -28978 FRAME_-28978_CENTER = 599 TKFRAME_-28978_SPEC = 'ANGLES' TKFRAME_-28978_RELATIVE = 'JUICE_JUPITER_BSM' TKFRAME_-28978_ANGLES = ( -1.8707, 0.0, 0.0 ) TKFRAME_-28978_AXES = ( 3, 2, 3 ) TKFRAME_-28978_UNITS = 'DEGREES' \begintext JUICE Jupiter-Sun-Orbit (JUICE_JSO) ------------------------------------------------------------------------ Definition: ----------- The Jupiter orbital frame is defined as follows: - +X axis is the position of the Sun relative to Jupiter; it's the primary vector and points from Jupiter to Sun; - +Y axis is the component of the inertially referenced velocity of Sun relative to Jupiter orthogonal to the +X axis; - +Z axis completes the right-handed system; - the origin of this frame is the center of mass of Jupiter. All vectors are geometric: no aberration corrections are used. Required Data: -------------- This frame is defined as a two-vector frame using two different types of specifications for the primary and secondary vectors. The primary vector is defined as an 'observer-target position' vector and the secondary vector is defined as an 'observer-target velocity' vector, therefore, the ephemeris data required to compute the Jupiter-Sun state vector in the J2000 reference frame must be loaded before using this frame. Remarks: -------- In the current version this frame duplicates the JUPITER_SUN_ORB frame in order to align the frame names with the JUNO mission [22]. This frame is defined based on SPK data: different planetary ephemerides for Jupiter, Sun and the Sun Barycenter will lead to a different frame orientation at a given time. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. JUICE_JSO using the DE405 ephemeris. \begindata FRAME_JUICE_JSO = -28979 FRAME_-28979_NAME = 'JUICE_JSO' FRAME_-28979_CLASS = 5 FRAME_-28979_CLASS_ID = -28979 FRAME_-28979_CENTER = 599 FRAME_-28979_RELATIVE = 'J2000' FRAME_-28979_DEF_STYLE = 'PARAMETERIZED' FRAME_-28979_FAMILY = 'TWO-VECTOR' FRAME_-28979_PRI_AXIS = 'X' FRAME_-28979_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_-28979_PRI_OBSERVER = 'JUPITER' FRAME_-28979_PRI_TARGET = 'SUN' FRAME_-28979_PRI_ABCORR = 'NONE' FRAME_-28979_SEC_AXIS = 'Y' FRAME_-28979_SEC_VECTOR_DEF = 'OBSERVER_TARGET_VELOCITY' FRAME_-28979_SEC_OBSERVER = 'JUPITER' FRAME_-28979_SEC_TARGET = 'SUN' FRAME_-28979_SEC_ABCORR = 'NONE' FRAME_-28979_SEC_FRAME = 'J2000' \begintext Jupiter Heliospheric Frame (JUICE_JH) ------------------------------------------------------------------------ Definition: ----------- The Jupiter heliospheric frame is defined, based on the definition provided in [15] for the solar equatorial frame, as follows: - +X axis is the position of the Sun relative to Jupiter; it's the primary vector and points from Jupiter to the Sun; - +Z axis is the component of the Sun's north pole of date orthogonal to the +X axis; - +Y axis completes the right-handed reference frame; - the origin of this frame is the center of mass of Jupiter. All vectors are geometric: no aberration corrections are used. Required Data: -------------- This frame is defined as a two-vector frame using two different types of specifications for the primary and secondary vectors. The primary vector is defined as an 'observer-target position' vector. Therefore, the ephemeris data required to compute the Jupiter-Sun vector in the J2000 reference frame must be loaded before using this frame. The primary vector is defined as a constant vector in the IAU_SUN frame, which is a PCK-based frame. Therefore a PCK file containing the orientation constants for the Sun must be loaded before using this frame. Remarks: -------- This frame is defined based on SPK data: different planetary ephemerides for Jupiter, Jupiter Barycenter, the Sun and the Solar System Barycenter will lead to a different frame orientation at a given time. This frame is also defined based on the IAU_SUN frame, whose evaluation is based on the data included in the loaded PCK file: different orientation constants for the Sun's spin axis will lead to a different frame orientation at a given time. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. JUICE_JH using the IAU 2009 constants and the DE405 ephemeris. \begindata FRAME_JUICE_JH = -28969 FRAME_-28969_NAME = 'JUICE_JH' FRAME_-28969_CLASS = 5 FRAME_-28969_CLASS_ID = -28969 FRAME_-28969_CENTER = 599 FRAME_-28969_RELATIVE = 'J2000' FRAME_-28969_DEF_STYLE = 'PARAMETERIZED' FRAME_-28969_FAMILY = 'TWO-VECTOR' FRAME_-28969_PRI_AXIS = 'X' FRAME_-28969_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_-28969_PRI_OBSERVER = 'JUPITER' FRAME_-28969_PRI_TARGET = 'SUN' FRAME_-28969_PRI_ABCORR = 'NONE' FRAME_-28969_SEC_AXIS = 'Z' FRAME_-28969_SEC_VECTOR_DEF = 'CONSTANT' FRAME_-28969_SEC_FRAME = 'IAU_SUN' FRAME_-28969_SEC_SPEC = 'RECTANGULAR' FRAME_-28969_SEC_VECTOR = ( 0, 0, 1 ) \begintext Jupiter Io Plasma Torus Frame (JUICE_IPT) ------------------------------------------------------------------------ SPICE frame name, common names and other designators: ----------------------------------------------------- Within the SPICE system, the JUICE Io Plasma Torus Frame is referred as JUICE_IPT. Definition: ----------- The JUICE Io Plasma Torus Frame frame is defined as follows (from [17]): - +Z axis is parallel to the centrifugal axis of epoch which is 2/3 of the angle of the rotational and magnetic axes of Jupiter; - +Y axis is defined with respect to the meridian where the magnetic and geographic equators cross at longitude 249.2 degrees in the System III Right-handed frame; - +X completes the right-handed frame; - the origin of this frame is the center of mass of Jupiter. Remarks: -------- The centrifugal axis is oriented at 2/3 of the angle between the rotational and magnetic axes helps define the centrifugal equator up to about Europa's distance, approximately. Beyond that the centrifugal equator tends to become parallel to the rotational equator, but that effect can only be included through magnetic field models – there is no analytical formulation-. Users should know that the JUICE_IPT frame should be limited to studies of the Io torus [24]. This frame is based on the VIP4 model (see [16]) using as reference the System III Right-handed body-fixed frame for Jupiter with the constants provided in the IAU 2009 report (see [19]) for Jupiter's north pole and primer meridian location. The magnetic system rotates with Jupiter at the same rate, but about the magnetic dipole instead of the Jovian spin axis. \begindata FRAME_JUICE_IPT = -28968 FRAME_-28968_NAME = 'JUICE_IPT' FRAME_-28968_CLASS = 4 FRAME_-28968_CLASS_ID = -28968 FRAME_-28968_CENTER = -28968 OBJECT_-28968_FRAME = 'JUICE_IPT' TKFRAME_-28968_SPEC = 'ANGLES' TKFRAME_-28968_RELATIVE = 'JUPITER_SYSTEM3RH_2009' TKFRAME_-28968_ANGLES = ( 0, -159.2, -6.3333333333 ) TKFRAME_-28968_AXES = ( 2, 3, 2 ) TKFRAME_-28968_UNITS = 'DEGREES' \begintext Jupiter Europa Plasma Torus Frame (JUICE_EPT) ------------------------------------------------------------------------ SPICE frame name, common names and other designators: ----------------------------------------------------- Within the SPICE system, the JUICE Europa Plasma Torus Frame is referred as JUICE_EPT. Definition: ----------- The JUICE Europa Plasma Torus Frame frame is defined as follows: - +Y axis is parallel to the vector normal to Europa orbital plane; - +X axis is parallel to the line Jupiter-Europa with origin at Jupiter; - +Z completes the right-handed frame; - the origin of this frame is located at 10.5 RJ (Radius of Jupiter) along Jupiter-Europa position vector. \begindata FRAME_JUICE_EPT = -28988 FRAME_-28988_NAME = 'JUICE_EPT' FRAME_-28988_CLASS = 5 FRAME_-28988_CLASS_ID = -28988 FRAME_-28988_CENTER = -28988 OBJECT_-28988_FRAME = 'JUICE_EPT' FRAME_-28988_RELATIVE = 'J2000' FRAME_-28988_DEF_STYLE = 'PARAMETERIZED' FRAME_-28988_FAMILY = 'TWO-VECTOR' FRAME_-28988_PRI_AXIS = 'X' FRAME_-28988_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_-28988_PRI_OBSERVER = 'EUROPA' FRAME_-28988_PRI_TARGET = 'JUPITER' FRAME_-28988_PRI_ABCORR = 'NONE' FRAME_-28988_SEC_AXIS = 'Y' FRAME_-28988_SEC_VECTOR_DEF = 'OBSERVER_TARGET_VELOCITY' FRAME_-28988_SEC_OBSERVER = 'EUROPA' FRAME_-28988_SEC_TARGET = 'JUPITER' FRAME_-28988_SEC_ABCORR = 'NONE' FRAME_-28988_SEC_FRAME = 'J2000' \begintext Jupiter Rings Frames ------------------------------------------------------------------------ SPICE frame name, common names and other designators: ----------------------------------------------------- Within the SPICE system, the JUICE Jupiter Rings reference frames are referred as JUICE_JUP_RING_BOUNDARY, JUICE_JUP_HALO_RING, JUICE_JUP_MAIN_RING, JUICE_JUP_AMA_GOS_RING, JUICE_JUP_THE_GOS_RING, and JUICE_JUP_THE_RING_EXT. Definition: ----------- The JUICE Jupiter Rings reference frames are coincident with the Jupiter body-fixed reference frame JUICE_JUPITER_IF_J2000. \begindata FRAME_JUICE_JUP_RING_BOUNDARY = -28940 FRAME_-28940_NAME = 'JUICE_JUP_RING_BOUNDARY' FRAME_-28940_CLASS = 4 FRAME_-28940_CLASS_ID = -28940 FRAME_-28940_CENTER = 599 TKFRAME_-28940_RELATIVE = 'JUICE_JUPITER_IF_J2000' TKFRAME_-28940_SPEC = 'ANGLES' TKFRAME_-28940_UNITS = 'DEGREES' TKFRAME_-28940_ANGLES = ( 0.0, 0.0, 0.0 ) TKFRAME_-28940_AXES = ( 2, 3, 2 ) FRAME_JUICE_JUP_HALO_RING = -28941 FRAME_-28941_NAME = 'JUICE_JUP_HALO_RING' FRAME_-28941_CLASS = 4 FRAME_-28941_CLASS_ID = -28941 FRAME_-28941_CENTER = -28941 OBJECT_-28941_FRAME = 'JUICE_JUP_HALO_RING' TKFRAME_-28941_RELATIVE = 'JUICE_JUPITER_IF_J2000' TKFRAME_-28941_SPEC = 'ANGLES' TKFRAME_-28941_UNITS = 'DEGREES' TKFRAME_-28941_ANGLES = ( 0.0, 0.0, 0.0 ) TKFRAME_-28941_AXES = ( 2, 3, 2 ) FRAME_JUICE_JUP_MAIN_RING = -28942 FRAME_-28942_NAME = 'JUICE_JUP_MAIN_RING' FRAME_-28942_CLASS = 4 FRAME_-28942_CLASS_ID = -28942 FRAME_-28942_CENTER = -28942 OBJECT_-28942_FRAME = 'JUICE_JUP_MAIN_RING' TKFRAME_-28942_RELATIVE = 'JUICE_JUPITER_IF_J2000' TKFRAME_-28942_SPEC = 'ANGLES' TKFRAME_-28942_UNITS = 'DEGREES' TKFRAME_-28942_ANGLES = ( 0.0, 0.0, 0.0 ) TKFRAME_-28942_AXES = ( 2, 3, 2 ) FRAME_JUICE_JUP_AMA_GOS_RING = -28943 FRAME_-28943_NAME = 'JUICE_JUP_AMA_GOS_RING' FRAME_-28943_CLASS = 4 FRAME_-28943_CLASS_ID = -28943 FRAME_-28943_CENTER = -28943 OBJECT_-28943_FRAME = 'JUICE_JUP_AMA_GOS_RING' TKFRAME_-28943_RELATIVE = 'JUICE_JUPITER_IF_J2000' TKFRAME_-28943_SPEC = 'ANGLES' TKFRAME_-28943_UNITS = 'DEGREES' TKFRAME_-28943_ANGLES = ( 0.0, 0.0, 0.0 ) TKFRAME_-28943_AXES = ( 2, 3, 2 ) FRAME_JUICE_JUP_THE_GOS_RING = -28944 FRAME_-28944_NAME = 'JUICE_JUP_THE_GOS_RING' FRAME_-28944_CLASS = 4 FRAME_-28944_CLASS_ID = -28944 FRAME_-28944_CENTER = -28944 OBJECT_-28944_FRAME = 'JUICE_JUP_THE_GOS_RING' TKFRAME_-28944_RELATIVE = 'JUICE_JUPITER_IF_J2000' TKFRAME_-28944_SPEC = 'ANGLES' TKFRAME_-28944_UNITS = 'DEGREES' TKFRAME_-28944_ANGLES = ( 0.0, 0.0, 0.0 ) TKFRAME_-28944_AXES = ( 2, 3, 2 ) FRAME_JUICE_JUP_THE_RING_EXT = -28945 FRAME_-28945_NAME = 'JUICE_JUP_THE_RING_EXT' FRAME_-28945_CLASS = 4 FRAME_-28945_CLASS_ID = -28945 FRAME_-28945_CENTER = -28945 OBJECT_-28945_FRAME = 'JUICE_JUP_THE_RING_EXT' TKFRAME_-28945_RELATIVE = 'JUICE_JUPITER_IF_J2000' TKFRAME_-28945_SPEC = 'ANGLES' TKFRAME_-28945_UNITS = 'DEGREES' TKFRAME_-28945_ANGLES = ( 0.0, 0.0, 0.0 ) TKFRAME_-28945_AXES = ( 2, 3, 2 ) \begintext Callisto-centered Phi Zorb frame (JUICE_CALLISTO_PHI_ORB) ------------------------------------------------------------------------ SPICE frame name, common names and other designators: ----------------------------------------------------- Within the SPICE system, and for the JUICE mission, the Callisto centered Phi Zorb frame is referred as JUICE_CALLISTO_PHI_ORB. In the documentation provided by the JUICE MAG team (see [21]), it is referred as Satellite centered Phi Zorb Coordinates or SPhiZ. Definition: ----------- The Callisto-centered Phi Zorb frame is defined as follows (from [21]): - Y axis is the position of the Jupiter relative to Callisto; it's the primary vector and points from Callisto to Jupiter; - -X axis is the component of the inertially referenced velocity of Jupiter relative to Callisto orthogonal to the +Y axis; - +Z axis completes the right-handed system; - the origin of this frame is the center of mass of Callisto. All vectors are geometric: no aberration corrections are used. Uses and applications: ---------------------- The Callisto-centered Phi Zorb frame is used to analyze Callisto data where the interactions between the plasma flow and Callisto's orbital motions are the processes of interest. Required Data: -------------- This frame is defined as a two-vector frame using two different types of specifications for the primary and secondary vectors. The primary vector is defined as an 'observer-target position' vector and the secondary vector is defined as an 'observer-target velocity' vector, therefore, the ephemeris data required to compute the Callisto-Jupiter state vector in the J2000 reference frame must be loaded before using this frame. Remarks: -------- This frame is a transformation of the CALLISTO_JUPITER_ORB frame. The transformation applied is x'=-y, y'=x, z'=z. This frame is defined based on SPK data: different planetary ephemerides for Callisto, Jupiter and the Jupiter Barycenter will lead to a different frame orientation at a given time. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. JUICE_CALLISTO_PHI_ORB using the DE405 ephemeris. \begindata FRAME_JUICE_CALLISTO_PHI_ORB = -28980 FRAME_-28980_NAME = 'JUICE_CALLISTO_PHI_ORB' FRAME_-28980_CLASS = 5 FRAME_-28980_CLASS_ID = -28980 FRAME_-28980_CENTER = 504 FRAME_-28980_RELATIVE = 'J2000' FRAME_-28980_DEF_STYLE = 'PARAMETERIZED' FRAME_-28980_FAMILY = 'TWO-VECTOR' FRAME_-28980_PRI_AXIS = 'Y' FRAME_-28980_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_-28980_PRI_OBSERVER = 'CALLISTO' FRAME_-28980_PRI_TARGET = 'JUPITER' FRAME_-28980_PRI_ABCORR = 'NONE' FRAME_-28980_SEC_AXIS = '-X' FRAME_-28980_SEC_VECTOR_DEF = 'OBSERVER_TARGET_VELOCITY' FRAME_-28980_SEC_OBSERVER = 'CALLISTO' FRAME_-28980_SEC_TARGET = 'JUPITER' FRAME_-28980_SEC_ABCORR = 'NONE' FRAME_-28980_SEC_FRAME = 'J2000' \begintext Europa-centered Phi Zorb frame (JUICE_EUROPA_PHI_ORB) ------------------------------------------------------------------------ SPICE frame name, common names and other designators: ----------------------------------------------------- Within the SPICE system, and for the JUICE mission, the Europa centered Phi Zorb frame is referred as JUICE_EUROPA_PHI_ORB. In the documentation provided by the JUICE MAG team (see [21]), it is referred as Satellite centered Phi Zorb Coordinates or SPhiZ. Definition: ----------- The Europa-centered Phi Zorb frame is defined as follows (from [21]): - +Y axis is the position of the Jupiter relative to Europa; it's the primary vector and points from Europa to Jupiter; - -X axis is the component of the inertially referenced velocity of Jupiter relative to Europa orthogonal to the +Y axis; - +Z axis completes the right-handed system; - the origin of this frame is the center of mass of Europa. All vectors are geometric: no aberration corrections are used. Uses and applications: ---------------------- The Europa-centered Phi Zorb frame is used to analyze Europa data where the interactions between the plasma flow and Europa's orbital motions are the processes of interest. Required Data: -------------- This frame is defined as a two-vector frame using two different types of specifications for the primary and secondary vectors. The primary vector is defined as an 'observer-target position' vector and the secondary vector is defined as an 'observer-target velocity' vector, therefore, the ephemeris data required to compute the Europa-Jupiter state vector in the J2000 reference frame must be loaded before using this frame. Remarks: -------- This frame is a transformation of the EUROPA_JUPITER_ORB frame. The transformation applied is x'=-y, y'=x, z'=z. This frame is defined based on SPK data: different planetary ephemerides for Europa, Jupiter and the Jupiter Barycenter will lead to a different frame orientation at a given time. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. JUICE_EUROPA_PHI_ORB using DE405 ephemeris. \begindata FRAME_JUICE_EUROPA_PHI_ORB = -28981 FRAME_-28981_NAME = 'JUICE_EUROPA_PHI_ORB' FRAME_-28981_CLASS = 5 FRAME_-28981_CLASS_ID = -28981 FRAME_-28981_CENTER = 502 FRAME_-28981_RELATIVE = 'J2000' FRAME_-28981_DEF_STYLE = 'PARAMETERIZED' FRAME_-28981_FAMILY = 'TWO-VECTOR' FRAME_-28981_PRI_AXIS = 'Y' FRAME_-28981_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_-28981_PRI_OBSERVER = 'EUROPA' FRAME_-28981_PRI_TARGET = 'JUPITER' FRAME_-28981_PRI_ABCORR = 'NONE' FRAME_-28981_SEC_AXIS = '-X' FRAME_-28981_SEC_VECTOR_DEF = 'OBSERVER_TARGET_VELOCITY' FRAME_-28981_SEC_OBSERVER = 'EUROPA' FRAME_-28981_SEC_TARGET = 'JUPITER' FRAME_-28981_SEC_ABCORR = 'NONE' FRAME_-28981_SEC_FRAME = 'J2000' \begintext Ganymede-centered Phi Zorb frame (JUICE_GANYMEDE_PHI_ORB) ------------------------------------------------------------------------ SPICE frame name, common names and other designators: ----------------------------------------------------- Within the SPICE system, and for the JUICE mission, the Ganymede centered Phi Zorb frame is referred as JUICE_GANYMEDE_PHI_ORB. In the documentation provided by the JUICE MAG team (see [21]), it is referred as Satellite centered Phi Zorb Coordinates or SPhiZ. Definition: ----------- The Ganymede-centered Phi Zorb frame is defined as follows (from [21]): - +Y axis is the position of the Jupiter relative to Ganymede; it's the primary vector and points from Ganymede to Jupiter; - -X axis is the component of the inertially referenced velocity of Jupiter relative to Ganymede orthogonal to the +Y axis; - +Z axis completes the right-handed system; - the origin of this frame is the center of mass of Ganymede. All vectors are geometric: no aberration corrections are used. Uses and applications: ---------------------- The Europa-centered Phi Zorb frame is used to analyze Europa data where the interactions between the plasma flow and Europa's orbital motions are the processes of interest. Required Data: -------------- This frame is defined as a two-vector frame using two different types of specifications for the primary and secondary vectors. The primary vector is defined as an 'observer-target position' vector and the secondary vector is defined as an 'observer-target velocity' vector, therefore, the ephemeris data required to compute the Ganymede-Jupiter state vector in the J2000 reference frame must be loaded before using this frame. Remarks: -------- This frame is a transformation of the EUROPA_JUPITER_ORB frame. The transformation applied is x'=-y, y'=x, z'=z. This frame is defined based on SPK data: different planetary ephemerides for Ganymede, Jupiter and the Jupiter Barycenter will lead to a different frame orientation at a given time. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. JUICE_GANYMEDE_PHI_ORB using the DE405 ephemeris. \begindata FRAME_JUICE_GANYMEDE_PHI_ORB = -28982 FRAME_-28982_NAME = 'JUICE_GANYMEDE_PHI_ORB' FRAME_-28982_CLASS = 5 FRAME_-28982_CLASS_ID = -28982 FRAME_-28982_CENTER = 503 FRAME_-28982_RELATIVE = 'J2000' FRAME_-28982_DEF_STYLE = 'PARAMETERIZED' FRAME_-28982_FAMILY = 'TWO-VECTOR' FRAME_-28982_PRI_AXIS = 'Y' FRAME_-28982_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_-28982_PRI_OBSERVER = 'GANYMEDE' FRAME_-28982_PRI_TARGET = 'JUPITER' FRAME_-28982_PRI_ABCORR = 'NONE' FRAME_-28982_SEC_AXIS = '-X' FRAME_-28982_SEC_VECTOR_DEF = 'OBSERVER_TARGET_VELOCITY' FRAME_-28982_SEC_OBSERVER = 'GANYMEDE' FRAME_-28982_SEC_TARGET = 'JUPITER' FRAME_-28982_SEC_ABCORR = 'NONE' FRAME_-28982_SEC_FRAME = 'J2000' \begintext Ganymede Inertial Frame at J2000 (JUICE_GANYMEDE_IF_J2000) ------------------------------------------------------------------------ Definition: ----------- The Ganymede Inertial Frame at J2000 is defined as follows: - +Z axis is parallel to Ganymede's rotation axis at J2000, pointing toward the North side of the invariable plane; - +X axis is aligned with the ascending node of the Ganymede orbital plane with the Jovian equator plane at J2000; - +Y axis completes the right-handed system; - the origin of this frame is the center of mass of Ganymede. All vectors are geometric: no aberration corrections are used. Remarks: -------- This frame is defined as a fixed offset frame using constant vectors as the specification method. The fixed offset for these vectors were based on the following directions (that also define a two-vector frame): - +Z axis along Right Ascension of 268.50683687347919 degrees and Declination of 64.436151398948965 of the Ganymede pole at J2000 epoch in J2000 inertial frame; - +X axis along Right Ascension of 171.92422396663190 degrees and Declination of 3.1386886718475613 with respect to J2000 inertial frame at J2000 epoch, which corresponds to the RA/DEC of the Ganymede instantaneous orbital plane ascending node on the Ganymede equator at J2000 epoch in J2000 inertial frame; This frame has been defined based on the IAU_GANYMEDE frame, whose evaluation was based on the data included in the loaded PCK file. When evaluated, the IAU 2009 constants for Ganymede (see [19]) were used. In addition jup310.bsp and noe-5-2017-gal-a-reduced.bsp have been used to compute the instantaneous orbital plane ascending node on the Ganymede equator at J2000 epoch in J2000 inertial frame. \begindata FRAME_JUICE_GANYMEDE_IF_J2000 = -28983 FRAME_-28983_NAME = 'JUICE_GANYMEDE_IF_J2000' FRAME_-28983_CLASS = 4 FRAME_-28983_CLASS_ID = -28983 FRAME_-28983_CENTER = 599 TKFRAME_-28983_SPEC = 'ANGLES' TKFRAME_-28983_RELATIVE = 'J2000' TKFRAME_-28983_ANGLES = ( -88.057204042707568 25.504190046604286 -48.968728165793905 ) TKFRAME_-28983_AXES = ( 3, 2, 3 ) TKFRAME_-28983_UNITS = 'DEGREES' \begintext Ganymede Magnetic Right-Handed (JUICE_GANYMEDE_MAG) ------------------------------------------------------------------------ SPICE frame name: ----------------------------------------------------- Within the SPICE system, the Ganymede Magnetic frame using the data from [25] is referred as JUICE_GANYMEDE_MAG. Definition: ----------- The Ganymede Magnetic frame is defined as follows (from [25]): - +Z axis is parallel to the magnetic dipole axis of epoch and aligned with the North magnetic pole of epoch; - +Y axis is defined with respect to the meridian where the magnetic and geographic equators cross at longitude 249.2 degrees in the IAU_GANYMEDE frame; - +X completes the right-handed frame; - the origin of this frame is the center of mass of Ganymede. Required Data: -------------- This frame is defined as a constant rotation with respect to the IAU_GANYMEDE body-fixed frame, which is a PCK-based frame. Therefore, a PCK file containing the orientation constants for Ganymede must be loaded before using this frame. Remarks: -------- This frame is base on the model in [25] using as reference the body-fixed frame for Ganymede provided in the loaded PCK kernel. The magnetic system rotates with Ganymede at the same rate, but about the magnetic dipole instead of the Ganymede spin axis. The north dipole location is the best-fit, centered dipole magnetic moment vector M direction in the IAU_GANYMEDE body-fixed frame. M is defined to be titled 175.69 degrees away from the Ganymede spin axis towards longitude 24.4 degrees West (24.24 deg from the Jupiter-facing meridian plane toward the moon's trailing hemisphere), therefore, the current values for the Ganymede north magnetic centered dipole planetocentric coordinates are: Longitude = 335.6 (degrees) Latitude = -85.69 (degrees) This coordinate system may prove useful for organizing in-situ charged particle measurements a low Ganymede altitudes and latitudes (~<30 deg) where Ganymede's dipole dominates that of Jupiter. \begindata FRAME_JUICE_GANYMEDE_MAG = -28984 FRAME_-28984_NAME = 'JUICE_GANYMEDE_MAG' FRAME_-28984_CLASS = 4 FRAME_-28984_CLASS_ID = -28997 FRAME_-28984_CENTER = 599 TKFRAME_-28984_SPEC = 'ANGLES' TKFRAME_-28984_RELATIVE = 'IAU_GANYMEDE' TKFRAME_-28984_ANGLES = ( 0, -335.6, -175.69 ) TKFRAME_-28984_AXES = ( 2, 3, 2 ) TKFRAME_-28984_UNITS = 'DEGREES' \begintext JUICE Heliocentric Radial-Tangential-Normal (JUICE_HGRTN) ------------------------------------------------------------------------ SPICE frame name, common names and other designators: ----------------------------------------------------- Within the SPICE system, the JUICE Heliocentric Radial-Tangential-Normal frame is referred as JUICE_HGRTN. In literature, this frame is referred as HGRTN (from [4], [6], [7], and [8]). Definition: ----------- The JUICE Heliocentric Radial-Tangential-Normal frame is defined as follows (from [4]): - the position of JUICE relative to the Sun is the primary vector: +X axis points from the Sun to JUICE; - the projection of the solar rotational axis perpendicular to the +X axis defines the frame's +Z axis; - +Y axis completes the right-handed system; - the origin of this frame is the center of mass of the Sun. All vectors are geometric: no aberration corrections are used. Uses and applications (from [6]): ---------------------------------- This frame is used to define the velocity and field direction of the plasma environment that the spacecraft finds itself in. Required Data: -------------- This frame is defined as a two-vector frame using two different types of specifications for the primary and secondary vectors. The primary vector is defined as an 'observer-target position' vector, therefore, the ephemeris data required to compute the Sun-JUICE position vector in the J2000 reference frame must be loaded before using this frame. The secondary vector is defined as a constant vector in the IAU_SUN frame, which is a PCK-based frame, therefore a PCK file containing the orientation constants for the Sun must be loaded before using this frame. Remarks: -------- This frame is defined based on SPK data: different planetary ephemerides for Jupiter, Jupiter's Barycenter, the Sun, the Solar System Barycenter and JUICE spacecraft will lead to different frame orientation at a given time. This frame is also defined based on the IAU_SUN frame, whose evaluation is based on the data included in the loaded PCK file: different orientation constants for the Sun's spin axis will lead to different frame orientation at a given time. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. JUICE_HGRTN using the IAU 2009 constants, the DE405 ephemeris and the JUICE ephemeris version N. \begindata FRAME_JUICE_HGRTN = -28990 FRAME_-28990_NAME = 'JUICE_HGRTN' FRAME_-28990_CLASS = 5 FRAME_-28990_CLASS_ID = -28990 FRAME_-28990_CENTER = 10 FRAME_-28990_RELATIVE = 'J2000' FRAME_-28990_DEF_STYLE = 'PARAMETERIZED' FRAME_-28990_FAMILY = 'TWO-VECTOR' FRAME_-28990_PRI_AXIS = 'X' FRAME_-28990_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_-28990_PRI_OBSERVER = 'SUN' FRAME_-28990_PRI_TARGET = 'JUICE' FRAME_-28990_PRI_ABCORR = 'NONE' FRAME_-28990_SEC_AXIS = 'Z' FRAME_-28990_SEC_VECTOR_DEF = 'CONSTANT' FRAME_-28990_SEC_FRAME = 'IAU_SUN' FRAME_-28990_SEC_SPEC = 'RECTANGULAR' FRAME_-28990_SEC_VECTOR = ( 0, 0, 1 ) \begintext Sun JUICE Radial-Tangential-Normal (JUICE_SUN_RTN) ------------------------------------------------------------------------ SPICE frame name, common names and other designators: ----------------------------------------------------- Within the SPICE system, the Sun JUICE Radial-Tangential-Normal frame is referred as JUICE_SUN_RTN. In literature, this frame is referred as RTN (from [4]), Orbit RTN Coordinate System (from [10]), or radial-transverse-normal (from [5]). Definition: ----------- The Sun JUICE Radial-Tangential-Normal frame is defined as follows (from [10]): - the position of Sun relative to JUICE is the primary vector: +X axis points from the JUICE to Sun; - the normal vector to the orbit plane defines the frame's +Z axis; - +Y axis completes the right-handed system; - the origin of this frame is the center of mass of JUICE. All vectors are geometric: no aberration corrections are used. Uses and applications (from [10]): ---------------------------------- This frame is used to project the perturbation forces imposed on the spacecraft so that the Gauss Lagrange equations can be established and the variations of the orbit elements expressed as function of the three components of the perturbation acceleration in the orbit radial (+X), tangential (+Y) and normal (+Z) axis. Required Data: -------------- This frame is defined as a two-vector frame using two different types of specifications for the primary and secondary vectors. The primary vector is defined as an 'observer-target position' vector and the secondary vector is defined as an 'observer-target velocity' vector, therefore, the ephemeris data required to compute the JUICE-Sun state vector in the J2000 reference frame must be loaded before using this frame. Remarks: -------- This frame is defined based on SPK data: different planetary ephemerides for Jupiter, Jupiter's Barycenter, the Sun, the Solar System Barycenter and JUICE spacecraft will lead to different frame orientation at a given time. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. JUICE_SUN_RTN using the DE405 ephemeris and the JUICE ephemeris version N. \begindata FRAME_JUICE_SUN_RTN = -28991 FRAME_-28991_NAME = 'JUICE_SUN_RTN' FRAME_-28991_CLASS = 5 FRAME_-28991_CLASS_ID = -28991 FRAME_-28991_CENTER = -28 FRAME_-28991_RELATIVE = 'J2000' FRAME_-28991_DEF_STYLE = 'PARAMETERIZED' FRAME_-28991_FAMILY = 'TWO-VECTOR' FRAME_-28991_PRI_AXIS = 'X' FRAME_-28991_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_-28991_PRI_OBSERVER = 'JUICE' FRAME_-28991_PRI_TARGET = 'SUN' FRAME_-28991_PRI_ABCORR = 'NONE' FRAME_-28991_SEC_AXIS = 'Y' FRAME_-28991_SEC_VECTOR_DEF = 'OBSERVER_TARGET_VELOCITY' FRAME_-28991_SEC_OBSERVER = 'JUICE' FRAME_-28991_SEC_TARGET = 'SUN' FRAME_-28991_SEC_ABCORR = 'NONE' FRAME_-28991_SEC_FRAME = 'J2000' \begintext JUICE Solar Equatorial Radial-Tangential-Normal (JUICE_SUN_EQU_RTN) ------------------------------------------------------------------------ SPICE frame name, common names and other designators: ----------------------------------------------------- Within the SPICE system, the JUICE Solar Equatorial Radial-Tangential-Normal frame is referred as JUICE_SUN_EQU_RTN. In literature, this frame is referred as HGRTN (from [4], [6], [7], and [8]). Definition: ----------- The JUICE Solar Equatorial Radial-Tangential-Normal frame is defined as follows (from [4]): - the position of JUICE relative to the Sun is the primary vector: +X axis points from the Sun to JUICE; - the projection of the solar rotational axis perpendicular to the +X axis defines the frame's +Z axis; - +Y axis completes the right-handed system; - the origin of this frame is the center of mass of JUICE. All vectors are geometric: no aberration corrections are used. Uses and applications (from [6]): ---------------------------------- This frame is used to define the velocity and field direction of the plasma environment that the spacecraft finds itself in. Required Data: -------------- This frame is defined as a two-vector frame using two different types of specifications for the primary and secondary vectors. The primary vector is defined as an 'observer-target position' vector, therefore, the ephemeris data required to compute the Sun-JUICE position vector in the J2000 reference frame must be loaded before using this frame. The secondary vector is defined as a constant vector in the IAU_SUN frame, which is a PCK-based frame, therefore a PCK file containing the orientation constants for the Sun must be loaded before using this frame. Remarks: -------- This frame is defined based on SPK data: different planetary ephemerides for Jupiter, Jupiter's Barycenter, the Sun, the Solar System Barycenter and JUICE spacecraft will lead to different frame orientation at a given time. This frame is also defined based on the IAU_SUN frame, whose evaluation is based on the data included in the loaded PCK file: different orientation constants for the Sun's spin axis will lead to different frame orientation at a given time. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. JUICE_SUN_EQU_RTN using the IAU 2009 constants, the DE405 ephemeris and the JUICE ephemeris version N. \begindata FRAME_JUICE_SUN_EQU_RTN = -28994 FRAME_-28994_NAME = 'JUICE_SUN_EQU_RTN' FRAME_-28994_CLASS = 5 FRAME_-28994_CLASS_ID = -28994 FRAME_-28994_CENTER = 10 FRAME_-28994_RELATIVE = 'J2000' FRAME_-28994_DEF_STYLE = 'PARAMETERIZED' FRAME_-28994_FAMILY = 'TWO-VECTOR' FRAME_-28994_PRI_AXIS = 'X' FRAME_-28994_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_-28994_PRI_OBSERVER = 'JUICE' FRAME_-28994_PRI_TARGET = 'JUICE' FRAME_-28994_PRI_ABCORR = 'NONE' FRAME_-28994_SEC_AXIS = 'Z' FRAME_-28994_SEC_VECTOR_DEF = 'CONSTANT' FRAME_-28994_SEC_FRAME = 'IAU_SUN' FRAME_-28994_SEC_SPEC = 'RECTANGULAR' FRAME_-28994_SEC_VECTOR = ( 0, 0, 1 ) \begintext Jupiter JUICE Dipole Meridian (JUICE_JUPITER_DM) ------------------------------------------------------------------------ SPICE frame name, common names and other designators: ----------------------------------------------------- Within the SPICE system, the Jupiter JUICE Dipole Meridian Frame frame is referred as JUICE_JUPITER_DM. In literature, this frame is referred as Jupiter DM (from [3] and [11]). Definition: ----------- The Jupiter JUICE Dipole Meridian frame is defined, based on the definition provided in [11] for the Earth's dipole meridian frame, as follows: - +Z axis is aligned with Jupiter's north magnetic pole; - the Y-axis is chosen to be perpendicular to a radius vector to the point of observation. The positive Y direction is chosen to be eastwards, so that the X-axis is directed outwards from Jupiter to JUICE. - the X-axis completes the right-handed system; - the origin of this frame is the center of mass of Jupiter. All vectors are geometric: no aberration corrections are used. Uses and applications (from [11]): ---------------------------------- It is used to order data controlled by the dipole magnetic field where the influence of the solar wind interaction with the magnetosphere is weak. It has been used extensively to describe the distortions of the magnetospheric field in terms of the two angles declination and inclination which can be easily derived from measurements in this frame. Required Data: -------------- This frame is defined as a two-vector frame using two different types of specifications for the primary and secondary vectors. The primary vector is defined as a constant vector in the JUPITER_MAG_VIP4 body-fixed frame, which provides the orientation for the Jupiter North magnetic dipole and the Jupiter magnetic frame with respect to the IAU_JUPITER body-fixed frame. The secondary vector is defined as an 'observer-target position' vector, therefore, the ephemeris data required to compute the Jupiter-JUICE position vector in the J2000 reference frame must be loaded before using this frame. Remarks: -------- This frame is defined based on SPK data: different planetary ephemerides for Jupiter, Jupiter's Barycenter and JUICE spacecraft will lead to different frame orientation at a given time. This frame is also defined based on the JUPITER_MAG_VIP4 frame, which is defined relative to the IAU_JUPITER frame, whose evaluation is based on the data included in the loaded PCK file: different orientation constants for Jupiter's spin axis will lead to different frame orientation at a given time. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. JUICE_JUPITER_DM using the IAU 2009 constants, the DE405 ephemeris and JUICE ephemeris version N. \begindata FRAME_JUICE_JUPITER_DM = -28992 FRAME_-28992_NAME = 'JUICE_JUPITER_DM' FRAME_-28992_CLASS = 5 FRAME_-28992_CLASS_ID = -28992 FRAME_-28992_CENTER = 599 FRAME_-28992_RELATIVE = 'J2000' FRAME_-28992_DEF_STYLE = 'PARAMETERIZED' FRAME_-28992_FAMILY = 'TWO-VECTOR' FRAME_-28992_PRI_AXIS = 'Z' FRAME_-28992_PRI_VECTOR_DEF = 'CONSTANT' FRAME_-28992_PRI_FRAME = 'JUPITER_MAG_VIP4' FRAME_-28992_PRI_SPEC = 'RECTANGULAR' FRAME_-28992_PRI_VECTOR = ( 0, 0, 1 ) FRAME_-28992_SEC_AXIS = 'X' FRAME_-28992_SEC_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_-28992_SEC_OBSERVER = 'JUPITER' FRAME_-28992_SEC_TARGET = 'JUICE' FRAME_-28992_SEC_ABCORR = 'NONE' \begintext JUICE Jupiter R-Theta-Phi (JUICE_JUPITER_RTP) ------------------------------------------------------------------------ SPICE frame name, common names and other designators: ----------------------------------------------------- Within the SPICE system, the JUICE Jupiter R-Theta-Phi frame is referred as JUICE_JUPITER_RTP. In literature, this frame is referred as Jupiter R-Theta-Phi, R-Theta-Phi or Radial-Down-Corotation ([20]). Definition: ----------- The JUICE Jupiter R-Theta-Phi is defined as follows: - +X axis is the position of JUICE relative to Jupiter; it is the primary vector and points from Jupiter's center to center of the spacecraft; - +Y axis is the component of Jupiter's south pole of date orthogonal to the +X axis; - +Z axis completes the right-handed system; it is parallel to the Jovian equator and positive in the direction of corotation. - the origin of this frame is the center of mass of Jupiter. All vectors are geometric: no aberration corrections are used. Required Data: -------------- This frame is defined as a two-vector frame using two different types of specifications for the primary and secondary vectors. The primary vector is defined as an 'observer-target position' vector, therefore, the ephemeris data required to compute the Jupiter-JUICE position vector in the J2000 reference frame must be loaded before using this frame. The secondary vector is defined as a constant vector in the IAU_JUPITER body-fixed frame, which is a PCK-based frame. Therefore a PCK file containing the orientation constants for Jupiter must be loaded before using this frame. Remarks: -------- This frame is defined based on SPK data: different planetary ephemerides for Jupiter, Jupiter Barycenter, and JUICE spacecraft will lead to a different frame orientation at a given time. This frame is also defined based on the IAU_JUPITER frame, whose evaluation is based on the data included in the loaded PCK file: different orientation constants for Jupiter's spin axis will lead to a different frame orientation at a given time. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. JUICE_JUPITER_RTPU using the IAU 2009 constants, the DE405 ephemeris and JUICE ephemeris version N. \begindata FRAME_JUICE_JUPITER_RTP = -28993 FRAME_-28993_NAME = 'JUICE_JUPITER_RTP' FRAME_-28993_CLASS = 5 FRAME_-28993_CLASS_ID = -28993 FRAME_-28993_CENTER = 599 FRAME_-28993_RELATIVE = 'J2000' FRAME_-28993_DEF_STYLE = 'PARAMETERIZED' FRAME_-28993_FAMILY = 'TWO-VECTOR' FRAME_-28993_PRI_AXIS = 'X' FRAME_-28993_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_-28993_PRI_OBSERVER = 'JUPITER' FRAME_-28993_PRI_TARGET = 'JUICE' FRAME_-28993_PRI_ABCORR = 'NONE' FRAME_-28993_SEC_AXIS = 'Y' FRAME_-28993_SEC_VECTOR_DEF = 'CONSTANT' FRAME_-28993_SEC_SPEC = 'RECTANGULAR' FRAME_-28993_SEC_VECTOR = ( 0.0, 0.0, -1.0 ) FRAME_-28993_SEC_FRAME = 'IAU_JUPITER' \begintext Jupiter Generic Frame Definitions ------------------------------------------------------------------------------ This section contains the definition of the Jupiter System generic frames. Jupiter System III Right-handed - IAU 1994 (JUPITER_SYSTEM3RH_1965) ------------------------------------------------------------------------ SPICE frame name, common names and other designators: ----------------------------------------------------- Within the SPICE system, the Jupiter System III Right-handed using IAU 1994 constants is referred as JUPITER_SYSTEM3RH_1965. In the documentation provided by the JUNO team (see [17]), this frame is referred as S3RH. Note that in the JUNO S3RH colatitude is used instead of latitude. Definition: ----------- The Jupiter System III Right-handed frame is defined as follows (from [14]): - +Z axis is parallel to Jupiter rotation axis, pointing toward the North side of the invariable plane; - +X axis is aligned with the ascending node of the Jovian orbital plane with the Jovian equator plane; - +Y axis completes the right-handed system; - the origin of this frame is the center of mass of Jupiter. Remarks: -------- This frame is defined as a PCK-based frame, using Jupiter's orientation data provided in the IAU 1994 report (see [18]). This frame is equivalent to the IAU_JUPITER body-fixed frame, when using pck00006.tpc. The orientation of this frame with respect to the J2000 inertial frame is provided using three Euler angles which describe the pole and prime meridian location: the first two angles, in order, are the right ascension and declination (RA and DEC) of the north pole of Jupiter as a function of time. The third angle is the prime meridian location (represented by 'PM'), which is expressed as a rotation about the north pole, also a function of time. The time arguments of functions that define orientation always refer to Barycentric Dynamical Time (TDB), measured in centuries or days past J2000 epoch, which is Julian ephemeris date 2451545.0. The time units are ephemeris days for prime meridian motion and ephemeris centuries for motion of the pole. In addition to the north pole and prime meridian location, the IAU 1994 report also provides the nutation precession angles for Jupiter's Barycenter, which is provided using the ``Nutation Precession Angles'' keyword. For further information about the nutation models used, please refer to section ``Models for Satellites in Text PCK Kernels'' in [1]. \begindata FRAME_JUPITER_SYSTEM3RH_1965 = -28999 FRAME_-28999_NAME = 'JUPITER_SYSTEM3RH_1965' FRAME_-28999_CLASS = 2 FRAME_-28999_CLASS_ID = -28999 FRAME_-28999_CENTER = 599 BODY-28999_POLE_RA = ( 268.05 -0.009 0. ) BODY-28999_POLE_DEC = ( 64.49 0.003 0. ) BODY-28999_PM = ( 284.95 870.536 0. ) BODY-28999_LONG_AXIS = ( 0. ) BODY-28999_NUT_PREC_ANGLES = ( 73.32 91472.9 24.62 45137.2 283.90 4850.7 355.80 1191.3 119.90 262.1 229.80 64.3 352.25 2382.6 113.35 6070.0 146.64 182945.8 49.24 90274.4 ) \begintext Jupiter System III Right-handed - IAU 2009 (JUPITER_SYSTEM3RH_2009) ------------------------------------------------------------------------ SPICE frame name, common names and other designators: ----------------------------------------------------- Within the SPICE system, the Jupiter System III Right-handed using IAU 2009 constants is referred as JUPITER_SYSTEM3RH_2009. In the documentation provided by the JUNO team (see [17]), this frame is referred as S3RH. Note that in the JUNO S3RH colatitude is used instead of latitude. Definition: ----------- The Jupiter System III Right-handed frame is defined as follows (from [14]): - +Z axis is parallel to Jupiter rotation axis, pointing toward the North side of the invariable plane; - +X axis is aligned with the ascending node of the Jovian orbital plane with the Jovian equator plane; - +Y axis completes the right-handed system; - the origin of this frame is the center of mass of Jupiter. Remarks: -------- This frame is defined as a PCK-based frame, using Jupiter's orientation data provided in the IAU 2009 report (see [19]). This frame is equivalent to the IAU_JUPITER body-fixed frame, when using pck00010.tpc. The orientation of this frame with respect to the J2000 inertial frame is provided using three Euler angles which describe the pole and prime meridian location: the first two angles, in order, are the right ascension and declination (RA and DEC) of the north pole of Jupiter as a function of time. The third angle is the prime meridian location (represented by 'PM'), which is expressed as a rotation about the north pole, also a function of time. The time arguments of functions that define orientation always refer to Barycentric Dynamical Time (TDB), measured in centuries or days past J2000 epoch, which is Julian ephemeris date 2451545.0. The time units are ephemeris days for prime meridian motion and ephemeris centuries for motion of the pole. In addition to the north pole and prime meridian location, the IAU 2009 report also provides the nutation precession angles for Jupiter's north pole and primer meridian location, and for Jupiter's Barycenter. For further information about the nutation models used, please refer to section ``Models for Satellites in Text PCK Kernels'' in [1]. \begindata FRAME_JUPITER_SYSTEM3RH_2009 = -28998 FRAME_-28998_NAME = 'JUPITER_SYSTEM3RH_2009' FRAME_-28998_CLASS = 2 FRAME_-28998_CLASS_ID = -28998 FRAME_-28998_CENTER = 599 BODY-28998_POLE_RA = ( 268.056595 -0.006499 0. ) BODY-28998_POLE_DEC = ( 64.495303 0.002413 0. ) BODY-28998_PM = ( 284.95 870.536000 0. ) BODY-28998_LONG_AXIS = ( 0. ) BODY-28998_NUT_PREC_RA = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.000117 0.000938 0.001432 0.000030 0.002150 ) BODY-28998_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.000050 0.000404 0.000617 -0.000013 0.000926 ) BODY-28998_NUT_PREC_PM = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.0 0.0 0.0 0.0 0.0 ) BODY-28998_NUT_PREC_ANGLES = ( 73.32 91472.9 24.62 45137.2 283.90 4850.7 355.80 1191.3 119.90 262.1 229.80 64.3 352.25 2382.6 113.35 6070.0 146.64 182945.8 49.24 90274.4 99.360714 4850.4046 175.895369 1191.9605 300.323162 262.5475 114.012305 6070.2476 49.511251 64.3000 ) \begintext Jupiter Magnetic System III - VIP4 model (JUPITER_MAG_VIP4) ------------------------------------------------------------------------ SPICE frame name, common names and other designators: ----------------------------------------------------- Within the SPICE system, the Jupiter Magnetic System III Right-handed frame using the VIP4 model is referred as JUPITER_MAG_VIP4. In documentation, this frame is commonly referred as Jupiter Magnetic, with Magnetic north pole obtained using the VIP4 model (see [16], and [17]). Definition: ----------- The Jupiter Magnetic System III Right-Handed frame is defined as follows (from [17]): - +Z axis is parallel to the magnetic dipole axis of epoch and aligned with the North magnetic pole of epoch; - +Y axis is defined with respect to the meridian where the magnetic and geographic equators cross at longitude 249.2 degrees in the System III Right-handed frame; - +X completes the right-handed frame; - the origin of this frame is the center of mass of Jupiter. Required Data: -------------- This frame is defined as a constant rotation with respect to the IAU_JUPITER body-fixed frame, which is a PCK-based frame. Therefore, a PCK file containing the orientation constants for Jupiter must be loaded before using this frame. Remarks: -------- This frame is base on the VIP4 model (see [16]) using as reference the System III Right-handed body-fixed frame for Jupiter provided in the loaded PCK kernel. The magnetic system rotates with Jupiter at the same rate, but about the magnetic dipole instead of the Jovian spin axis. The north dipole location is the best-fit, centered dipole magnetic moment vector M direction in the IAU_JUPITER body-fixed frame based on the VIP4 model. M is defined to be titled 9.50 degrees away from the Jovian spin axis towards longitude 200.8 degrees West, therefore, the current values for the Jupiter north magnetic centered dipole planetocentric coordinates are: Longitude = 159.2 (degrees) Latitude = 80.5 (degrees) This frame is provided as the ``most generic'' Jupiter Magnetic System III Right-handed frame since the user has the possibility of loading different Jupiter orientation constants that would help to define different implementations of this frame. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. JUPITER_MAG_VIP4 using the IAU 2009 constants. \begindata FRAME_JUPITER_MAG_VIP4 = -28997 FRAME_-28997_NAME = 'JUPITER_MAG_VIP4' FRAME_-28997_CLASS = 4 FRAME_-28997_CLASS_ID = -28997 FRAME_-28997_CENTER = 599 TKFRAME_-28997_SPEC = 'ANGLES' TKFRAME_-28997_RELATIVE = 'IAU_JUPITER' TKFRAME_-28997_ANGLES = ( 0, -159.2, -9.5 ) TKFRAME_-28997_AXES = ( 2, 3, 2 ) TKFRAME_-28997_UNITS = 'DEGREES' \begintext Jupiter Mean Equator of Date Frame (JUPITER_MEQUD) ------------------------------------------------------------------------ Definition: ----------- The Jupiter mean equator of date frame is defined as follows: - X-Y plane is defined by Jupiter equator of date, with the +Z axis, the primary vector, parallel to Jupiter rotation axis of date, pointing toward the North side of the invariable plane; - +X axis is the component of the ascending node of Jupiter equator of date on the Earth Mean Equator of J2000 orthogonal to the +Z axis; - +Y axis completes the right-handed system; - the origin of this frame is the center of mass of Jupiter. All vectors are geometric: no aberration corrections are used. Required Data: -------------- This frame is defined as a two-vector frame using constant vectors as the specification method. The primary vector is defined as a constant vector in the IAU_JUPITER body-fixed frame, which is a PCK-based frame. Therefore, a PCK file containing the orientation constants for Jupiter must be loaded before using this frame. The secondary vector is defined in the J2000 reference frame and therefore it does not require any additional data. Remarks: -------- This frame is defined based on the IAU_JUPITER frame, whose evaluation is based on the data included in the loaded PCK file: different orientation constants for the spin axis of Jupiter will lead to a different frame orientation at a given time. This frame is provided as the ``most generic'' Jupiter mean equator of date frame since the user has the possibility of loading different Jupiter orientation constants that would help to define different implementations of this frame. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. JUPITER_MEQUD using the IAU 2009 constants. \begindata FRAME_JUPITER_MEQUD = 500599000 FRAME_500599000_NAME = 'JUPITER_MEQUD' FRAME_500599000_CLASS = 5 FRAME_500599000_CLASS_ID = 500599000 FRAME_500599000_CENTER = 599 FRAME_500599000_RELATIVE = 'J2000' FRAME_500599000_DEF_STYLE = 'PARAMETERIZED' FRAME_500599000_FAMILY = 'TWO-VECTOR' FRAME_500599000_PRI_AXIS = 'Z' FRAME_500599000_PRI_VECTOR_DEF = 'CONSTANT' FRAME_500599000_PRI_FRAME = 'IAU_JUPITER' FRAME_500599000_PRI_SPEC = 'RECTANGULAR' FRAME_500599000_PRI_VECTOR = ( 0, 0, 1 ) FRAME_500599000_SEC_AXIS = 'Y' FRAME_500599000_SEC_VECTOR_DEF = 'CONSTANT' FRAME_500599000_SEC_FRAME = 'J2000' FRAME_500599000_SEC_SPEC = 'RECTANGULAR' FRAME_500599000_SEC_VECTOR = ( 0, 0, 1 ) \begintext Jupiter Solar Equatorial Frame (JUPITER_SUN_EQU) ------------------------------------------------------------------------ Definition: ----------- The Jupiter solar equatorial frame is defined, based on the definition provided in [15] for the solar equatorial frame, as follows: - +X axis is the position of the Sun relative to Jupiter; it's the primary vector and points from Jupiter to the Sun; - +Z axis is the component of the Sun's north pole of date orthogonal to the +X axis; - +Y axis completes the right-handed reference frame; - the origin of this frame is the center of mass of Jupiter. All vectors are geometric: no aberration corrections are used. Required Data: -------------- This frame is defined as a two-vector frame using two different types of specifications for the primary and secondary vectors. The primary vector is defined as an 'observer-target position' vector. Therefore, the ephemeris data required to compute the Jupiter-Sun vector in the J2000 reference frame must be loaded before using this frame. The primary vector is defined as a constant vector in the IAU_SUN frame, which is a PCK-based frame. Therefore a PCK file containing the orientation constants for the Sun must be loaded before using this frame. Remarks: -------- This frame is defined based on SPK data: different planetary ephemerides for Jupiter, Jupiter Barycenter, the Sun and the Solar System Barycenter will lead to a different frame orientation at a given time. This frame is also defined based on the IAU_SUN frame, whose evaluation is based on the data included in the loaded PCK file: different orientation constants for the Sun's spin axis will lead to a different frame orientation at a given time. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. JUPITER_SUN_EQU using the IAU 2009 constants and the DE405 ephemeris. \begindata FRAME_JUPITER_SUN_EQU = 500599001 FRAME_500599001_NAME = 'JUPITER_SUN_EQU' FRAME_500599001_CLASS = 5 FRAME_500599001_CLASS_ID = 500599001 FRAME_500599001_CENTER = 599 FRAME_500599001_RELATIVE = 'J2000' FRAME_500599001_DEF_STYLE = 'PARAMETERIZED' FRAME_500599001_FAMILY = 'TWO-VECTOR' FRAME_500599001_PRI_AXIS = 'X' FRAME_500599001_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_500599001_PRI_OBSERVER = 'JUPITER' FRAME_500599001_PRI_TARGET = 'SUN' FRAME_500599001_PRI_ABCORR = 'NONE' FRAME_500599001_SEC_AXIS = 'Z' FRAME_500599001_SEC_VECTOR_DEF = 'CONSTANT' FRAME_500599001_SEC_FRAME = 'IAU_SUN' FRAME_500599001_SEC_SPEC = 'RECTANGULAR' FRAME_500599001_SEC_VECTOR = ( 0, 0, 1 ) \begintext Jupiter Orbital Frame (JUPITER_SUN_ORB) ------------------------------------------------------------------------ Definition: ----------- The Jupiter orbital frame is defined as follows: - +X axis is the position of the Sun relative to Jupiter; it's the primary vector and points from Jupiter to Sun; - +Y axis is the component of the inertially referenced velocity of Sun relative to Jupiter orthogonal to the +X axis; - +Z axis completes the right-handed system; - the origin of this frame is the center of mass of Jupiter. All vectors are geometric: no aberration corrections are used. Required Data: -------------- This frame is defined as a two-vector frame using two different types of specifications for the primary and secondary vectors. The primary vector is defined as an 'observer-target position' vector and the secondary vector is defined as an 'observer-target velocity' vector, therefore, the ephemeris data required to compute the Jupiter-Sun state vector in the J2000 reference frame must be loaded before using this frame. Remarks: -------- This frame is defined based on SPK data: different planetary ephemerides for Jupiter, Sun and the Sun Barycenter will lead to a different frame orientation at a given time. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. JUPITER_SUN_ORB using the DE405 ephemeris. \begindata FRAME_JUPITER_SUN_ORB = 500599002 FRAME_500599002_NAME = 'JUPITER_SUN_ORB' FRAME_500599002_CLASS = 5 FRAME_500599002_CLASS_ID = 500599002 FRAME_500599002_CENTER = 599 FRAME_500599002_RELATIVE = 'J2000' FRAME_500599002_DEF_STYLE = 'PARAMETERIZED' FRAME_500599002_FAMILY = 'TWO-VECTOR' FRAME_500599002_PRI_AXIS = 'X' FRAME_500599002_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_500599002_PRI_OBSERVER = 'JUPITER' FRAME_500599002_PRI_TARGET = 'SUN' FRAME_500599002_PRI_ABCORR = 'NONE' FRAME_500599002_SEC_AXIS = 'Y' FRAME_500599002_SEC_VECTOR_DEF = 'OBSERVER_TARGET_VELOCITY' FRAME_500599002_SEC_OBSERVER = 'JUPITER' FRAME_500599002_SEC_TARGET = 'SUN' FRAME_500599002_SEC_ABCORR = 'NONE' FRAME_500599002_SEC_FRAME = 'J2000' \begintext Jupiter-Centric Callisto-Following Frame (JUPITER_CALLISTO_BCSF) ------------------------------------------------------------------------ Definition: ----------- The Jupiter-centric Callisto-following frame is defined as follows: - X-Y plane is defined by the Jupiter's orbital plane of date with the +Z axis, the primary vector and the normal vector to this plane, always pointing toward the north side of the invariable plane; - +X axis is the component of the position of Callisto relative to Jupiter that is orthogonal to the +Z axis; - +Y axis completes the right-handed system; - the origin of this frame is the center of mass of Jupiter. All vectors are geometric: no aberration corrections are used. Required Data: -------------- The frame is defined as a two-vector frame using two different types of specifications for the primary and secondary vectors. The primary vector is defined as a constant vector in the JUPITER_SUN_ORB (Jupiter orbital) frame, which is a dynamic frame. Therefore, the data required to evaluate that base frame at the requested epoch must be loaded before using this frame. The secondary vector is defined as an 'observer-target position' vector. Therefore, the ephemeris data required to compute the Jupiter-Callisto vector in the J2000 reference frame must be loaded before using this frame. Remarks: -------- SPICE imposes a constraint in the definition of dynamic frames (see [1]): When the definition of a parameterized dynamic frame F1 refers to a second frame F2 the referenced frame F2 may be dynamic, but F2 must not make reference to any dynamic frame. Therefore, no other dynamic frame should make reference to this frame. This frame is defined based on SPK data: different planetary ephemerides for Callisto, Jupiter, Jupiter Barycenter, the Sun and the Solar System will lead to a different frame orientation at a given time. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. JUPITER_CALLISTO_BCSF using the DE405 ephemeris. \begindata FRAME_JUPITER_CALLISTO_BCSF = 500599006 FRAME_500599006_NAME = 'JUPITER_CALLISTO_BCSF' FRAME_500599006_CLASS = 5 FRAME_500599006_CLASS_ID = 500599006 FRAME_500599006_CENTER = 599 FRAME_500599006_RELATIVE = 'J2000' FRAME_500599006_DEF_STYLE = 'PARAMETERIZED' FRAME_500599006_FAMILY = 'TWO-VECTOR' FRAME_500599006_PRI_AXIS = 'Z' FRAME_500599006_PRI_VECTOR_DEF = 'CONSTANT' FRAME_500599006_PRI_FRAME = 'JUPITER_SUN_ORB' FRAME_500599006_PRI_SPEC = 'RECTANGULAR' FRAME_500599006_PRI_VECTOR = ( 0, 0, 1 ) FRAME_500599006_SEC_AXIS = 'X' FRAME_500599006_SEC_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_500599006_SEC_OBSERVER = 'JUPITER' FRAME_500599006_SEC_TARGET = 'CALLISTO' FRAME_500599006_SEC_ABCORR = 'NONE' \begintext Jupiter-Centric Europa-Following Frame (JUPITER_EUROPA_BCSF) ------------------------------------------------------------------------ Definition: ----------- The Jupiter-centric Europa-following frame is defined as follows: - X-Y plane is defined by the Jupiter's orbital plane of date with the +Z axis, the primary vector and the normal vector to this plane, always pointing toward the north side of the invariable plane; - +X axis is the component of the position of Europa relative to Jupiter that is orthogonal to the +Z axis; - +Y axis completes the right-handed system; - the origin of this frame is the center of mass of Jupiter. All vectors are geometric: no aberration corrections are used. Required Data: -------------- The frame is defined as a two-vector frame using two different types of specifications for the primary and secondary vectors. The primary vector is defined as a constant vector in the JUPITER_SUN_ORB (Jupiter orbital) frame, which is a dynamic frame. Therefore, the data required to evaluate that base frame at the requested epoch must be loaded before using this frame. The secondary vector is defined as an 'observer-target position' vector. Therefore, the ephemeris data required to compute the Europa-Jupiter vector in the J2000 reference frame must be loaded before using this frame. Remarks: -------- SPICE imposes a constraint in the definition of dynamic frames (see [1]): When the definition of a parameterized dynamic frame F1 refers to a second frame F2 the referenced frame F2 may be dynamic, but F2 must not make reference to any dynamic frame. Therefore, no other dynamic frame should make reference to this frame. This frame is defined based on SPK data: different planetary ephemerides for Europa, Jupiter, Jupiter Barycenter, the Sun and the Solar System will lead to a different frame orientation at a given time. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. JUPITER_EUROPA_BCSF using the DE405 ephemeris. \begindata FRAME_JUPITER_EUROPA_BCSF = 500599004 FRAME_500599004_NAME = 'JUPITER_EUROPA_BCSF' FRAME_500599004_CLASS = 5 FRAME_500599004_CLASS_ID = 500599004 FRAME_500599004_CENTER = 599 FRAME_500599004_RELATIVE = 'J2000' FRAME_500599004_DEF_STYLE = 'PARAMETERIZED' FRAME_500599004_FAMILY = 'TWO-VECTOR' FRAME_500599004_PRI_AXIS = 'Z' FRAME_500599004_PRI_VECTOR_DEF = 'CONSTANT' FRAME_500599004_PRI_FRAME = 'JUPITER_SUN_ORB' FRAME_500599004_PRI_SPEC = 'RECTANGULAR' FRAME_500599004_PRI_VECTOR = ( 0, 0, 1 ) FRAME_500599004_SEC_AXIS = 'X' FRAME_500599004_SEC_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_500599004_SEC_OBSERVER = 'JUPITER' FRAME_500599004_SEC_TARGET = 'EUROPA' FRAME_500599004_SEC_ABCORR = 'NONE' \begintext Jupiter-Centric Ganymede-Following Frame (JUPITER_GANYMEDE_BCSF) ------------------------------------------------------------------------ Definition: ----------- The Jupiter-centric Ganymede-following frame is defined as follows: - X-Y plane is defined by the Jupiter's orbital plane of date with the +Z axis, the primary vector and the normal vector to this plane, always pointing toward the north side of the invariable plane; - +X axis is the component of the position of Ganymede relative to Jupiter that is orthogonal to the +Z axis; - +Y axis completes the right-handed system; - the origin of this frame is the center of mass of Jupiter. All vectors are geometric: no aberration corrections are used. Required Data: -------------- The frame is defined as a two-vector frame using two different types of specifications for the primary and secondary vectors. The primary vector is defined as a constant vector in the JUPITER_SUN_ORB (Jupiter orbital) frame, which is a dynamic frame. Therefore, the data required to evaluate that base frame at the requested epoch must be loaded before using this frame. The secondary vector is defined as an 'observer-target position' vector. Therefore, the ephemeris data required to compute the Ganymede-Jupiter vector in the J2000 reference frame must be loaded before using this frame. Remarks: -------- SPICE imposes a constraint in the definition of dynamic frames (see [1]): When the definition of a parameterized dynamic frame F1 refers to a second frame F2 the referenced frame F2 may be dynamic, but F2 must not make reference to any dynamic frame. Therefore, no other dynamic frame should make reference to this frame. This frame is defined based on SPK data: different planetary ephemerides for Ganymede, Jupiter, Jupiter Barycenter, the Sun and the Solar System will lead to a different frame orientation at a given time. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. JUPITER_GANYMEDE_BCSF using the DE405 ephemeris. \begindata FRAME_JUPITER_GANYMEDE_BCSF = 500599005 FRAME_500599005_NAME = 'JUPITER_GANYMEDE_BCSF' FRAME_500599005_CLASS = 5 FRAME_500599005_CLASS_ID = 500599005 FRAME_500599005_CENTER = 599 FRAME_500599005_RELATIVE = 'J2000' FRAME_500599005_DEF_STYLE = 'PARAMETERIZED' FRAME_500599005_FAMILY = 'TWO-VECTOR' FRAME_500599005_PRI_AXIS = 'Z' FRAME_500599005_PRI_VECTOR_DEF = 'CONSTANT' FRAME_500599005_PRI_FRAME = 'JUPITER_SUN_ORB' FRAME_500599005_PRI_SPEC = 'RECTANGULAR' FRAME_500599005_PRI_VECTOR = ( 0, 0, 1 ) FRAME_500599005_SEC_AXIS = 'X' FRAME_500599005_SEC_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_500599005_SEC_OBSERVER = 'JUPITER' FRAME_500599005_SEC_TARGET = 'GANYMEDE' FRAME_500599005_SEC_ABCORR = 'NONE' \begintext Callisto Orbital Frame (CALLISTO_JUPITER_ORB) ------------------------------------------------------------------------ Definition: ----------- The Callisto orbital frame is defined as follows: - +X axis is the position of the Jupiter relative to Callisto; it's the primary vector and points from Callisto to Jupiter; - +Y axis is the component of the inertially referenced velocity of Jupiter relative to Callisto orthogonal to the +X axis; - +Z axis completes the right-handed system; - the origin of this frame is the center of mass of Callisto. All vectors are geometric: no aberration corrections are used. Required Data: -------------- This frame is defined as a two-vector frame using two different types of specifications for the primary and secondary vectors. The primary vector is defined as an 'observer-target position' vector and the secondary vector is defined as an 'observer-target velocity' vector, therefore, the ephemeris data required to compute the Callisto-Jupiter state vector in the J2000 reference frame must be loaded before using this frame. Remarks: -------- This frame is defined based on SPK data: different planetary ephemerides for Callisto, Jupiter and the Jupiter Barycenter will lead to a different frame orientation at a given time. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. CALLISTO_JUPITER_ORB using the DE405 ephemeris. \begindata FRAME_CALLISTO_JUPITER_ORB = 500504000 FRAME_500504000_NAME = 'CALLISTO_JUPITER_ORB' FRAME_500504000_CLASS = 5 FRAME_500504000_CLASS_ID = 500504000 FRAME_500504000_CENTER = 504 FRAME_500504000_RELATIVE = 'J2000' FRAME_500504000_DEF_STYLE = 'PARAMETERIZED' FRAME_500504000_FAMILY = 'TWO-VECTOR' FRAME_500504000_PRI_AXIS = 'X' FRAME_500504000_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_500504000_PRI_OBSERVER = 'CALLISTO' FRAME_500504000_PRI_TARGET = 'JUPITER' FRAME_500504000_PRI_ABCORR = 'NONE' FRAME_500504000_SEC_AXIS = 'Y' FRAME_500504000_SEC_VECTOR_DEF = 'OBSERVER_TARGET_VELOCITY' FRAME_500504000_SEC_OBSERVER = 'CALLISTO' FRAME_500504000_SEC_TARGET = 'JUPITER' FRAME_500504000_SEC_ABCORR = 'NONE' FRAME_500504000_SEC_FRAME = 'J2000' \begintext Europa Orbital Frame (EUROPA_JUPITER_ORB) ------------------------------------------------------------------------ Definition: ----------- The Europa orbital frame is defined as follows: - +X axis is the position of the Jupiter relative to Europa; it's the primary vector and points from Europa to Jupiter; - +Y axis is the component of the inertially referenced velocity of Jupiter relative to Europa orthogonal to the +X axis; - +Z axis completes the right-handed system; - the origin of this frame is the center of mass of Europa. All vectors are geometric: no aberration corrections are used. Required Data: -------------- This frame is defined as a two-vector frame using two different types of specifications for the primary and secondary vectors. The primary vector is defined as an 'observer-target position' vector and the secondary vector is defined as an 'observer-target velocity' vector, therefore, the ephemeris data required to compute the Europa-Jupiter state vector in the J2000 reference frame must be loaded before using this frame. Remarks: -------- This frame is defined based on SPK data: different planetary ephemerides for Europa, Jupiter and the Jupiter Barycenter will lead to a different frame orientation at a given time. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. EUROPA_JUPITER_ORB using the DE405 ephemeris. \begindata FRAME_EUROPA_JUPITER_ORB = 500502000 FRAME_500502000_NAME = 'EUROPA_JUPITER_ORB' FRAME_500502000_CLASS = 5 FRAME_500502000_CLASS_ID = 500502000 FRAME_500502000_CENTER = 502 FRAME_500502000_RELATIVE = 'J2000' FRAME_500502000_DEF_STYLE = 'PARAMETERIZED' FRAME_500502000_FAMILY = 'TWO-VECTOR' FRAME_500502000_PRI_AXIS = 'X' FRAME_500502000_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_500502000_PRI_OBSERVER = 'EUROPA' FRAME_500502000_PRI_TARGET = 'JUPITER' FRAME_500502000_PRI_ABCORR = 'NONE' FRAME_500502000_SEC_AXIS = 'Y' FRAME_500502000_SEC_VECTOR_DEF = 'OBSERVER_TARGET_VELOCITY' FRAME_500502000_SEC_OBSERVER = 'EUROPA' FRAME_500502000_SEC_TARGET = 'JUPITER' FRAME_500502000_SEC_ABCORR = 'NONE' FRAME_500502000_SEC_FRAME = 'J2000' \begintext Ganymede Orbital Frame (GANYMEDE_JUPITER_ORB) ------------------------------------------------------------------------ Definition: ----------- The Ganymede orbital frame is defined as follows: - +X axis is the position of the Jupiter relative to Ganymede; it's the primary vector and points from Ganymede to Jupiter; - +Y axis is the component of the inertially referenced velocity of Jupiter relative to Ganymede orthogonal to the +X axis; - +Z axis completes the right-handed system; - the origin of this frame is the center of mass of Ganymede. All vectors are geometric: no aberration corrections are used. Required Data: -------------- This frame is defined as a two-vector frame using two different types of specifications for the primary and secondary vectors. The primary vector is defined as an 'observer-target position' vector and the secondary vector is defined as an 'observer-target velocity' vector, therefore, the ephemeris data required to compute the Ganymede-Jupiter state vector in the J2000 reference frame must be loaded before using this frame. Remarks: -------- This frame is defined based on SPK data: different planetary ephemerides for Ganymede, Jupiter and the Jupiter Barycenter will lead to a different frame orientation at a given time. It is strongly recommended to indicate what data have been used in the evaluation of this frame when referring to it, e.g. GANYMEDE_JUPITER_ORB using the DE405 ephemeris. \begindata FRAME_GANYMEDE_JUPITER_ORB = 500503000 FRAME_500503000_NAME = 'GANYMEDE_JUPITER_ORB' FRAME_500503000_CLASS = 5 FRAME_500503000_CLASS_ID = 500503000 FRAME_500503000_CENTER = 503 FRAME_500503000_RELATIVE = 'J2000' FRAME_500503000_DEF_STYLE = 'PARAMETERIZED' FRAME_500503000_FAMILY = 'TWO-VECTOR' FRAME_500503000_PRI_AXIS = 'X' FRAME_500503000_PRI_VECTOR_DEF = 'OBSERVER_TARGET_POSITION' FRAME_500503000_PRI_OBSERVER = 'GANYMEDE' FRAME_500503000_PRI_TARGET = 'JUPITER' FRAME_500503000_PRI_ABCORR = 'NONE' FRAME_500503000_SEC_AXIS = 'Y' FRAME_500503000_SEC_VECTOR_DEF = 'OBSERVER_TARGET_VELOCITY' FRAME_500503000_SEC_OBSERVER = 'GANYMEDE' FRAME_500503000_SEC_TARGET = 'JUPITER' FRAME_500503000_SEC_ABCORR = 'NONE' FRAME_500503000_SEC_FRAME = 'J2000' \begintext JUICE Natural Bodies NAIF ID Codes -- Definitions ============================================================================== This section contains name to NAIF ID mappings for the natural bodies of the JUICE mission. Once the contents of this file is loaded into the KERNEL POOL, these mappings become available within SPICE, making it possible to use names instead of ID code in the high level SPICE routine calls. Jupiter Satellites: ------------------- This table presents the JUICE Jupiter Satellites names and IDs Name ID Synonyms --------------------- ------- -------------------------- IO 501 IO EUROPA 502 EU, EUR GANYMEDE 503 GA, GAN CALLISTO 504 CA, CAL AMALTHEA 505 AMA HIMALIA 506 HIM ELARA 507 ELA PASIPHAE 508 PAS SINOPE 509 SIN LYSITHEA 510 LYS CARME 511 CAR ANANKE 512 ANA LEDA 513 LED THEBE 514 THE ADRASTEA 515 ADR METIS 516 MET CALLIRRHOE 517 CLH THEMISTO 518 THM MEGACLITE 519 MEG TAYGETE 520 TAY CHALDENE 521 CHA HARPALYKE 522 HAR KALYKE 523 KLK IOCASTE 524 IOC ERINOME 525 ERI ISONOE 526 ISO PRAXIDIKE 527 PRA AUTONOE 528 AUT THYONE 529 THY HERMIPPE 530 HER AITNE 531 AIT EURYDOME 532 EYD EUANTHE 533 EUA EUPORIE 534 EUP ORTHOSIE 535 ORT SPONDE 536 SPO KALE 537 KLE PASITHEE 538 PST HEGEMONE 539 HEG MNEME 540 MNE AOEDE 541 AOE THELXINOE 542 TLX ARCHE 543 ARC KALLICHORE 544 KCH HELIKE 545 HLK CARPO 546 CRP EUKELADE 547 EUK CYLLENE 548 CYL KORE 549 KOR HERSE 550 HRS S2010_J1 551 S/2010_J_1, 10J1 S2010_J2 552 S/2010_J_2, 10J2 DIA 553 DIA S2016_J1 554 S/2016_J_1, 16J1 S2003_J18 555 S/2003_J_18, 3J18 S2011_J2 556 S/2011_J_2, 11J2 EIRENE 557 EIR PHILOPHROSYNE 558 PHI S2017_J1 559 S/2017_J_1, 17J1 EUPHEME 560 EPH S2003_J19 561 S/2003_J_19, 3J19 VALETUDO 562 VAL S2017_J2 563 S/2017_J_2, 17J2 S2017_J3 564 S/2017_J_3, 17J3 PANDIA 565 PDI S2017_J5 566 S/2017_J_5, 17J5 S2017_J6 567 S/2017_J_6, 17J6 S2017_J7 568 S/2017_J_7, 17J7 S2017_J8 569 S/2017_J_8, 17J8 S2017_J9 570 S/2017_J_9, 17J9 ERSA 571 ERS S2011_J1 572 S/2011_J_1, 11J1 S2003_J2 55501 S/2003_J_2, 3J2 S2003_J4 55502 S/2003_J_4, 3J4 S2003_J9 55503 S/2003_J_9, 3J9 S2003_J10 55504 S/2003_J_10, 3J10 S2003_J12 55505 S/2003_J_12, 3J12 S2003_J16 55506 S/2003_J_16, 3J16 S2003_J23 55507 S/2003_J_23, 3J23 S2003_J24 55508 S/2003_J_24, 3J24 The mappings summarized in this table are implemented by the keywords below. \begindata NAIF_BODY_CODE += ( 501 ) NAIF_BODY_NAME += ( 'IO' ) NAIF_BODY_CODE += ( 502 ) NAIF_BODY_NAME += ( 'EU' ) NAIF_BODY_CODE += ( 502 ) NAIF_BODY_NAME += ( 'EUR' ) NAIF_BODY_CODE += ( 502 ) NAIF_BODY_NAME += ( 'EUROPA' ) NAIF_BODY_CODE += ( 503 ) NAIF_BODY_NAME += ( 'GA' ) NAIF_BODY_CODE += ( 503 ) NAIF_BODY_NAME += ( 'GAN' ) NAIF_BODY_CODE += ( 503 ) NAIF_BODY_NAME += ( 'GANYMEDE' ) NAIF_BODY_CODE += ( 504 ) NAIF_BODY_NAME += ( 'CA' ) NAIF_BODY_CODE += ( 504 ) NAIF_BODY_NAME += ( 'CAL' ) NAIF_BODY_CODE += ( 504 ) NAIF_BODY_NAME += ( 'CALLISTO' ) NAIF_BODY_CODE += ( 505 ) NAIF_BODY_NAME += ( 'AMA' ) NAIF_BODY_CODE += ( 505 ) NAIF_BODY_NAME += ( 'AMALTHEA' ) NAIF_BODY_CODE += ( 506 ) NAIF_BODY_NAME += ( 'HIM' ) NAIF_BODY_CODE += ( 506 ) NAIF_BODY_NAME += ( 'HIMALIA' ) NAIF_BODY_CODE += ( 507 ) NAIF_BODY_NAME += ( 'ELA' ) NAIF_BODY_CODE += ( 507 ) NAIF_BODY_NAME += ( 'ELARA' ) NAIF_BODY_CODE += ( 508 ) NAIF_BODY_NAME += ( 'PAS' ) NAIF_BODY_CODE += ( 508 ) NAIF_BODY_NAME += ( 'PASIPHAE' ) NAIF_BODY_CODE += ( 509 ) NAIF_BODY_NAME += ( 'SIN' ) NAIF_BODY_CODE += ( 509 ) NAIF_BODY_NAME += ( 'SINOPE' ) NAIF_BODY_CODE += ( 510 ) NAIF_BODY_NAME += ( 'LYS' ) NAIF_BODY_CODE += ( 510 ) NAIF_BODY_NAME += ( 'LYSITHEA' ) NAIF_BODY_CODE += ( 511 ) NAIF_BODY_NAME += ( 'CAR' ) NAIF_BODY_CODE += ( 511 ) NAIF_BODY_NAME += ( 'CARME' ) NAIF_BODY_CODE += ( 512 ) NAIF_BODY_NAME += ( 'ANA' ) NAIF_BODY_CODE += ( 512 ) NAIF_BODY_NAME += ( 'ANANKE' ) NAIF_BODY_CODE += ( 513 ) NAIF_BODY_NAME += ( 'LED' ) NAIF_BODY_CODE += ( 513 ) NAIF_BODY_NAME += ( 'LEDA' ) NAIF_BODY_CODE += ( 514 ) NAIF_BODY_NAME += ( 'THE' ) NAIF_BODY_CODE += ( 514 ) NAIF_BODY_NAME += ( 'THEBE' ) NAIF_BODY_CODE += ( 515 ) NAIF_BODY_NAME += ( 'ADR' ) NAIF_BODY_CODE += ( 515 ) NAIF_BODY_NAME += ( 'ADRASTEA' ) NAIF_BODY_CODE += ( 516 ) NAIF_BODY_NAME += ( 'MET' ) NAIF_BODY_CODE += ( 516 ) NAIF_BODY_NAME += ( 'METIS' ) NAIF_BODY_CODE += ( 517 ) NAIF_BODY_NAME += ( 'CLH' ) NAIF_BODY_CODE += ( 517 ) NAIF_BODY_NAME += ( 'CALLIRRHOE' ) NAIF_BODY_CODE += ( 518 ) NAIF_BODY_NAME += ( 'THM' ) NAIF_BODY_CODE += ( 518 ) NAIF_BODY_NAME += ( 'THEMISTO' ) NAIF_BODY_CODE += ( 519 ) NAIF_BODY_NAME += ( 'MEG' ) NAIF_BODY_CODE += ( 519 ) NAIF_BODY_NAME += ( 'MEGACLITE' ) NAIF_BODY_CODE += ( 520 ) NAIF_BODY_NAME += ( 'TAY' ) NAIF_BODY_CODE += ( 520 ) NAIF_BODY_NAME += ( 'TAYGETE' ) NAIF_BODY_CODE += ( 521 ) NAIF_BODY_NAME += ( 'CHA' ) NAIF_BODY_CODE += ( 521 ) NAIF_BODY_NAME += ( 'CHALDENE' ) NAIF_BODY_CODE += ( 522 ) NAIF_BODY_NAME += ( 'HAR' ) NAIF_BODY_CODE += ( 522 ) NAIF_BODY_NAME += ( 'HARPALYKE' ) NAIF_BODY_CODE += ( 523 ) NAIF_BODY_NAME += ( 'KLK' ) NAIF_BODY_CODE += ( 523 ) NAIF_BODY_NAME += ( 'KALYKE' ) NAIF_BODY_CODE += ( 524 ) NAIF_BODY_NAME += ( 'IOC' ) NAIF_BODY_CODE += ( 524 ) NAIF_BODY_NAME += ( 'IOCASTE' ) NAIF_BODY_CODE += ( 525 ) NAIF_BODY_NAME += ( 'ERI' ) NAIF_BODY_CODE += ( 525 ) NAIF_BODY_NAME += ( 'ERINOME' ) NAIF_BODY_CODE += ( 526 ) NAIF_BODY_NAME += ( 'ISO' ) NAIF_BODY_CODE += ( 526 ) NAIF_BODY_NAME += ( 'ISONOE' ) NAIF_BODY_CODE += ( 527 ) NAIF_BODY_NAME += ( 'PRA' ) NAIF_BODY_CODE += ( 527 ) NAIF_BODY_NAME += ( 'PRAXIDIKE' ) NAIF_BODY_CODE += ( 528 ) NAIF_BODY_NAME += ( 'AUT' ) NAIF_BODY_CODE += ( 528 ) NAIF_BODY_NAME += ( 'AUTONOE' ) NAIF_BODY_CODE += ( 529 ) NAIF_BODY_NAME += ( 'THY' ) NAIF_BODY_CODE += ( 529 ) NAIF_BODY_NAME += ( 'THYONE' ) NAIF_BODY_CODE += ( 530 ) NAIF_BODY_NAME += ( 'HER' ) NAIF_BODY_CODE += ( 530 ) NAIF_BODY_NAME += ( 'HERMIPPE' ) NAIF_BODY_CODE += ( 531 ) NAIF_BODY_NAME += ( 'AIT' ) NAIF_BODY_CODE += ( 531 ) NAIF_BODY_NAME += ( 'AITNE' ) NAIF_BODY_CODE += ( 532 ) NAIF_BODY_NAME += ( 'EYD' ) NAIF_BODY_CODE += ( 532 ) NAIF_BODY_NAME += ( 'EURYDOME' ) NAIF_BODY_CODE += ( 533 ) NAIF_BODY_NAME += ( 'EUA' ) NAIF_BODY_CODE += ( 533 ) NAIF_BODY_NAME += ( 'EUANTHE' ) NAIF_BODY_CODE += ( 534 ) NAIF_BODY_NAME += ( 'EUP' ) NAIF_BODY_CODE += ( 534 ) NAIF_BODY_NAME += ( 'EUPORIE' ) NAIF_BODY_CODE += ( 535 ) NAIF_BODY_NAME += ( 'ORT' ) NAIF_BODY_CODE += ( 535 ) NAIF_BODY_NAME += ( 'ORTHOSIE' ) NAIF_BODY_CODE += ( 536 ) NAIF_BODY_NAME += ( 'SPO' ) NAIF_BODY_CODE += ( 536 ) NAIF_BODY_NAME += ( 'SPONDE' ) NAIF_BODY_CODE += ( 537 ) NAIF_BODY_NAME += ( 'KLE' ) NAIF_BODY_CODE += ( 537 ) NAIF_BODY_NAME += ( 'KALE' ) NAIF_BODY_CODE += ( 538 ) NAIF_BODY_NAME += ( 'PST' ) NAIF_BODY_CODE += ( 538 ) NAIF_BODY_NAME += ( 'PASITHEE' ) NAIF_BODY_CODE += ( 539 ) NAIF_BODY_NAME += ( 'HEG' ) NAIF_BODY_CODE += ( 539 ) NAIF_BODY_NAME += ( 'HEGEMONE' ) NAIF_BODY_CODE += ( 540 ) NAIF_BODY_NAME += ( 'MNE' ) NAIF_BODY_CODE += ( 540 ) NAIF_BODY_NAME += ( 'MNEME' ) NAIF_BODY_CODE += ( 541 ) NAIF_BODY_NAME += ( 'AOE' ) NAIF_BODY_CODE += ( 541 ) NAIF_BODY_NAME += ( 'AOEDE' ) NAIF_BODY_CODE += ( 542 ) NAIF_BODY_NAME += ( 'TLX' ) NAIF_BODY_CODE += ( 542 ) NAIF_BODY_NAME += ( 'THELXINOE' ) NAIF_BODY_CODE += ( 543 ) NAIF_BODY_NAME += ( 'ARC' ) NAIF_BODY_CODE += ( 543 ) NAIF_BODY_NAME += ( 'ARCHE' ) NAIF_BODY_CODE += ( 544 ) NAIF_BODY_NAME += ( 'KCH' ) NAIF_BODY_CODE += ( 544 ) NAIF_BODY_NAME += ( 'KALLICHORE' ) NAIF_BODY_CODE += ( 545 ) NAIF_BODY_NAME += ( 'HLK' ) NAIF_BODY_CODE += ( 545 ) NAIF_BODY_NAME += ( 'HELIKE' ) NAIF_BODY_CODE += ( 546 ) NAIF_BODY_NAME += ( 'CRP' ) NAIF_BODY_CODE += ( 546 ) NAIF_BODY_NAME += ( 'CARPO' ) NAIF_BODY_CODE += ( 547 ) NAIF_BODY_NAME += ( 'EUK' ) NAIF_BODY_CODE += ( 547 ) NAIF_BODY_NAME += ( 'EUKELADE' ) NAIF_BODY_CODE += ( 548 ) NAIF_BODY_NAME += ( 'CYL' ) NAIF_BODY_CODE += ( 548 ) NAIF_BODY_NAME += ( 'CYLLENE' ) NAIF_BODY_CODE += ( 549 ) NAIF_BODY_NAME += ( 'KOR' ) NAIF_BODY_CODE += ( 549 ) NAIF_BODY_NAME += ( 'KORE' ) NAIF_BODY_CODE += ( 550 ) NAIF_BODY_NAME += ( 'HRS' ) NAIF_BODY_CODE += ( 550 ) NAIF_BODY_NAME += ( 'HERSE' ) NAIF_BODY_CODE += ( 551 ) NAIF_BODY_NAME += ( '10J1' ) NAIF_BODY_CODE += ( 551 ) NAIF_BODY_NAME += ( 'S/2010_J_1' ) NAIF_BODY_CODE += ( 551 ) NAIF_BODY_NAME += ( 'S2010_J1' ) NAIF_BODY_CODE += ( 552 ) NAIF_BODY_NAME += ( '10J2' ) NAIF_BODY_CODE += ( 552 ) NAIF_BODY_NAME += ( 'S/2010_J_2' ) NAIF_BODY_CODE += ( 552 ) NAIF_BODY_NAME += ( 'S2010_J2' ) NAIF_BODY_CODE += ( 553 ) NAIF_BODY_NAME += ( 'DIA' ) NAIF_BODY_CODE += ( 553 ) NAIF_BODY_NAME += ( 'DIA' ) NAIF_BODY_CODE += ( 554 ) NAIF_BODY_NAME += ( '16J1' ) NAIF_BODY_CODE += ( 554 ) NAIF_BODY_NAME += ( 'S/2016_J_1' ) NAIF_BODY_CODE += ( 554 ) NAIF_BODY_NAME += ( 'S2016_J1' ) NAIF_BODY_CODE += ( 555 ) NAIF_BODY_NAME += ( '3J18' ) NAIF_BODY_CODE += ( 555 ) NAIF_BODY_NAME += ( 'S/2003_J_18' ) NAIF_BODY_CODE += ( 555 ) NAIF_BODY_NAME += ( 'S2003_J18' ) NAIF_BODY_CODE += ( 556 ) NAIF_BODY_NAME += ( '11J2' ) NAIF_BODY_CODE += ( 556 ) NAIF_BODY_NAME += ( 'S/2011_J_2' ) NAIF_BODY_CODE += ( 556 ) NAIF_BODY_NAME += ( 'S2011_J2' ) NAIF_BODY_CODE += ( 557 ) NAIF_BODY_NAME += ( 'EIR' ) NAIF_BODY_CODE += ( 557 ) NAIF_BODY_NAME += ( 'EIRENE' ) NAIF_BODY_CODE += ( 558 ) NAIF_BODY_NAME += ( 'PHI' ) NAIF_BODY_CODE += ( 558 ) NAIF_BODY_NAME += ( 'PHILOPHROSYNE' ) NAIF_BODY_CODE += ( 559 ) NAIF_BODY_NAME += ( '17J1' ) NAIF_BODY_CODE += ( 559 ) NAIF_BODY_NAME += ( 'S/2017_J_1' ) NAIF_BODY_CODE += ( 559 ) NAIF_BODY_NAME += ( 'S2017_J1' ) NAIF_BODY_CODE += ( 560 ) NAIF_BODY_NAME += ( 'EPH' ) NAIF_BODY_CODE += ( 560 ) NAIF_BODY_NAME += ( 'EUPHEME' ) NAIF_BODY_CODE += ( 561 ) NAIF_BODY_NAME += ( '3J19' ) NAIF_BODY_CODE += ( 561 ) NAIF_BODY_NAME += ( 'S/2003_J_19' ) NAIF_BODY_CODE += ( 561 ) NAIF_BODY_NAME += ( 'S2003_J19' ) NAIF_BODY_CODE += ( 562 ) NAIF_BODY_NAME += ( 'VAL' ) NAIF_BODY_CODE += ( 562 ) NAIF_BODY_NAME += ( 'VALETUDO' ) NAIF_BODY_CODE += ( 563 ) NAIF_BODY_NAME += ( '17J2' ) NAIF_BODY_CODE += ( 563 ) NAIF_BODY_NAME += ( 'S/2017_J_2' ) NAIF_BODY_CODE += ( 563 ) NAIF_BODY_NAME += ( 'S2017_J2' ) NAIF_BODY_CODE += ( 564 ) NAIF_BODY_NAME += ( '17J3' ) NAIF_BODY_CODE += ( 564 ) NAIF_BODY_NAME += ( 'S/2017_J_3' ) NAIF_BODY_CODE += ( 564 ) NAIF_BODY_NAME += ( 'S2017_J3' ) NAIF_BODY_CODE += ( 565 ) NAIF_BODY_NAME += ( 'PDI' ) NAIF_BODY_CODE += ( 565 ) NAIF_BODY_NAME += ( 'PANDIA' ) NAIF_BODY_CODE += ( 566 ) NAIF_BODY_NAME += ( '17J5' ) NAIF_BODY_CODE += ( 566 ) NAIF_BODY_NAME += ( 'S/2017_J_5' ) NAIF_BODY_CODE += ( 566 ) NAIF_BODY_NAME += ( 'S2017_J5' ) NAIF_BODY_CODE += ( 567 ) NAIF_BODY_NAME += ( '17J6' ) NAIF_BODY_CODE += ( 567 ) NAIF_BODY_NAME += ( 'S/2017_J_6' ) NAIF_BODY_CODE += ( 567 ) NAIF_BODY_NAME += ( 'S2017_J6' ) NAIF_BODY_CODE += ( 568 ) NAIF_BODY_NAME += ( '17J7' ) NAIF_BODY_CODE += ( 568 ) NAIF_BODY_NAME += ( 'S/2017_J_7' ) NAIF_BODY_CODE += ( 568 ) NAIF_BODY_NAME += ( 'S2017_J7' ) NAIF_BODY_CODE += ( 569 ) NAIF_BODY_NAME += ( '17J8' ) NAIF_BODY_CODE += ( 569 ) NAIF_BODY_NAME += ( 'S/2017_J_8' ) NAIF_BODY_CODE += ( 569 ) NAIF_BODY_NAME += ( 'S2017_J8' ) NAIF_BODY_CODE += ( 570 ) NAIF_BODY_NAME += ( '17J9' ) NAIF_BODY_CODE += ( 570 ) NAIF_BODY_NAME += ( 'S/2017_J_9' ) NAIF_BODY_CODE += ( 570 ) NAIF_BODY_NAME += ( 'S2017_J9' ) NAIF_BODY_CODE += ( 571 ) NAIF_BODY_NAME += ( 'ERS' ) NAIF_BODY_CODE += ( 571 ) NAIF_BODY_NAME += ( 'ERSA' ) NAIF_BODY_CODE += ( 572 ) NAIF_BODY_NAME += ( '11J1' ) NAIF_BODY_CODE += ( 572 ) NAIF_BODY_NAME += ( 'S/2011_J_1' ) NAIF_BODY_CODE += ( 572 ) NAIF_BODY_NAME += ( 'S2011_J1' ) NAIF_BODY_CODE += ( 55501 ) NAIF_BODY_NAME += ( '3J2' ) NAIF_BODY_CODE += ( 55501 ) NAIF_BODY_NAME += ( 'S/2003_J_2' ) NAIF_BODY_CODE += ( 55501 ) NAIF_BODY_NAME += ( 'S2003_J2' ) NAIF_BODY_CODE += ( 55502 ) NAIF_BODY_NAME += ( '3J4' ) NAIF_BODY_CODE += ( 55502 ) NAIF_BODY_NAME += ( 'S/2003_J_4' ) NAIF_BODY_CODE += ( 55502 ) NAIF_BODY_NAME += ( 'S2003_J4' ) NAIF_BODY_CODE += ( 55503 ) NAIF_BODY_NAME += ( '3J9' ) NAIF_BODY_CODE += ( 55503 ) NAIF_BODY_NAME += ( 'S/2003_J_9' ) NAIF_BODY_CODE += ( 55503 ) NAIF_BODY_NAME += ( 'S2003_J9' ) NAIF_BODY_CODE += ( 55504 ) NAIF_BODY_NAME += ( '3J10' ) NAIF_BODY_CODE += ( 55504 ) NAIF_BODY_NAME += ( 'S/2003_J_10' ) NAIF_BODY_CODE += ( 55504 ) NAIF_BODY_NAME += ( 'S2003_J10' ) NAIF_BODY_CODE += ( 55505 ) NAIF_BODY_NAME += ( '3J12' ) NAIF_BODY_CODE += ( 55505 ) NAIF_BODY_NAME += ( 'S/2003_J_12' ) NAIF_BODY_CODE += ( 55505 ) NAIF_BODY_NAME += ( 'S2003_J12' ) NAIF_BODY_CODE += ( 55506 ) NAIF_BODY_NAME += ( '3J16' ) NAIF_BODY_CODE += ( 55506 ) NAIF_BODY_NAME += ( 'S/2003_J_16' ) NAIF_BODY_CODE += ( 55506 ) NAIF_BODY_NAME += ( 'S2003_J16' ) NAIF_BODY_CODE += ( 55507 ) NAIF_BODY_NAME += ( '3J23' ) NAIF_BODY_CODE += ( 55507 ) NAIF_BODY_NAME += ( 'S/2003_J_23' ) NAIF_BODY_CODE += ( 55507 ) NAIF_BODY_NAME += ( 'S2003_J23' ) NAIF_BODY_CODE += ( 55508 ) NAIF_BODY_NAME += ( '3J24' ) NAIF_BODY_CODE += ( 55508 ) NAIF_BODY_NAME += ( 'S/2003_J_24' ) NAIF_BODY_CODE += ( 55508 ) NAIF_BODY_NAME += ( 'S2003_J24' ) \begintext Natural Bodies Models: ---------------------- This table presents the JUICE Natural Bodies Models names and IDs Name ID Synonyms ------------------------- ------ -------------------------- JUICE_IO_PLASMA_TORUS -28968 JUICE_EUROPA_PLASMA_TORUS -28988 JUICE_JUP_RING_BOUNDARY -28940 JUICE_JUP_HALO_RING -28941 JUICE_JUP_MAIN_RING -28942 JUICE_JUP_AMA_GOS_RING -28943 JUICE_JUP_THE_GOS_RING -28944 JUICE_JUP_THE_RING_EXT -28945 The mappings summarized in this table are implemented by the keywords below. \begindata NAIF_BODY_NAME += ( 'JUICE_IO_PLASMA_TORUS' ) NAIF_BODY_CODE += ( -28968 ) NAIF_BODY_NAME += ( 'JUICE_EUROPA_PLASMA_TORUS' ) NAIF_BODY_CODE += ( -28988 ) NAIF_BODY_NAME += ( 'JUICE_JUP_RING_BOUNDARY' ) NAIF_BODY_CODE += ( -28940 ) NAIF_BODY_NAME += ( 'JUICE_JUP_HALO_RING' ) NAIF_BODY_CODE += ( -28941 ) NAIF_BODY_NAME += ( 'JUICE_JUP_MAIN_RING' ) NAIF_BODY_CODE += ( -28942 ) NAIF_BODY_NAME += ( 'JUICE_JUP_AMA_GOS_RING' ) NAIF_BODY_CODE += ( -28943 ) NAIF_BODY_NAME += ( 'JUICE_JUP_THE_GOS_RING' ) NAIF_BODY_CODE += ( -28944 ) NAIF_BODY_NAME += ( 'JUICE_JUP_THE_RING_EXT' ) NAIF_BODY_CODE += ( -28945 ) \begintext End of FK file.