Preliminary TGO trajectory for March launch window, covering Cruise, 
Mars Orbit Insertion and first months in orbit before aerobraking.

This is a baseline NOT yet confirmed by Flight Dynamics.

#### NOTE THAT BODY ID IS *WRONG*, IT SHOULD BE -607 for ExoMars TGO #####


Two kernels for the March Launch Period Open and Close (LPO/LPC):
--------------------------------------------------------------------------      
Summary for: tgolpo.bsp
Body: -900
      Start of Interval (ET)              End of Interval (ET)
      -----------------------------       -----------------------------
      2016 MAR 13 20:14:09.185            2017 JAN 24 03:17:03.102
--------------------------------------------------------------------------      
Summary for: tgolpc.bsp
Body: -900
      Start of Interval (ET)              End of Interval (ET)
      -----------------------------       -----------------------------
      2016 MAR 24 21:36:03.185            2017 JAN 24 02:21:25.861
--------------------------------------------------------------------------      



On 17/12/2015 09:20, Michael.Khan@esa.int wrote:
> Alejandro
>
> The Delta-CReMA is long obsolete, but there is a new trajectory file that was produced by Flight Dynamics. 
> Please find it attached to this mail. In fact, I attach both the onbe for LPO (first day in the launch period) 
> and for LPC (last day in the launch period). As you state you can work with both OEM or SPK, I attach the 
> Spice Kernel, because that's the I have right now. I would have to produce the OEM. 
>
> The Spice Kernel starts at launcher separation and goes until before the start of aerobraking.
>
> Michael Khan