I am trying to propagate an orbit using the mission analysis block

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Haider
Haider 2025-11-17，6:25
评论： William Rose 2025-11-17，16:43
I am initially finding out the orbital parameters for the injection point and successively the drifts that I am gonna encounter and my final result needs to a fully High precision orbit incoporating drag and atmospheric model and also calculating revisit time at the same time calculating the orbital parameters variation. I am also doing a keplerian unperturbed analysis.

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