orbit elements problem

[justwant121]

I am confused about the coordinate system transformation mentioned in the paper. Is there a way for the author to convert the orbital six-element state vector in the paper into the more commonly used Keplerian six-element state vector? Thank you.

[talhazaidi13]

Yes you can use the Keplerian six-element state vector by following the same algorithm, it totally depends upon the dynamic model you are using. We followed the dynamic model provided in https://soar.wichita.edu/items/ec51485d-47fd-4531-bc3e-c8f451a40de9.