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

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.

[William Rose]

@Haider, what is your question? Please share your work thus far.