MagicConch
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Hi, I managed to do this however I've noticed that the RA and dec have some offsets about 5 degrees and declination by about half a degree of what they should be, any idea what could cause this?
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Hi everyone, I have the position of a satellite in cartesian coordinates measured in the ECEF frame (i.e. the position of the satellite is given in [x,y,z] coordinates with the Earth-center at the origin) and I want to convert this to and RA and Dec position as seen by the observer (topocentric frame). Can anyone help? Thanks!