Summary for: ExoMars_Crema_refCruiseTraj.bsp
 
Body: -660
      Start of Interval (ET)              End of Interval (ET)
      -----------------------------       -----------------------------
      2016 JAN 15 01:51:52.501            2016 OCT 20 18:41:50.971

Date Created: 9/30/2011
Notes: This is a cruise trajectory generated in MALTO to best match the ESA CReMA mission design.
(Body ID had not been set to -699 at the time this file was generated.  File can be regenerated if needed)


Summary for: ExoMars_ESA_Aerobraking_161104-170603_v3.bsp
 
Body: -699
      Start of Interval (ET)              End of Interval (ET)
      -----------------------------       -----------------------------
      2016 NOV 04 10:38:16.782            2017 JUN 03 19:47:39.155

Date Created: 1/24/2012
Notes: Aerobraking trajectory file generated from state vectors provided by ESA on 10/5/2011


Summary for: ExoMars_2yr_ScienceOrbit_reftraj_v2.bsp
 
Body: -699
      Start of Interval (ET)              End of Interval (ET)
      -----------------------------       -----------------------------
      2017 JUN 30 09:15:01.000            2019 JUN 30 09:15:01.000

Date Created:12/29/2011
Notes: Morbiter_v3.1 ExoMars 2 year science orbit reference trajectory. Includes 33x33 gravity field. No Sun, Atmospheric Drag, or SRP