Keplerian elements different in Spacecraft setup and Summary

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Keplerian elements different in Spacecraft setup and Summary

Postby oeren » Tue Jan 12, 2016 1:45 am

Hello,

Something I never got for GMAT was that, after an ElapsedSec propagation, the Command Summary tells me a completely different RAAN and AOP than I set up in Spacecraft properties. It's keeping me from finishing a mission design. Can anyone help?
oeren
 
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