The above question may sound naive. I am trying to understand how satellite ground track can be computed when satellite position and velocity vectors are available from on-board GPS receiver of a low earth orbiting satellite.
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Here is half of the answer - the other half is converting from ECEF to ECI. – Chris Sep 07 '16 at 15:22
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@ Chris I got the conversion from ECI state vectors to keplerian elements. But how to convert state vector ECEF frame to ECI frame. – Soumajit Sep 12 '16 at 15:17