TEME of Epoch—In this approach, the epoch of the TEME frame is held constant. Subsequent rotation matrices must therefore account for the change in precession and nutation from the epoch of the TEME frame to the epoch of the transformation.
orbit - Can someone explain to me the TEME reference frame in defining ...
I have TEME coordinates from sgp4 propagation. I can convert those (in python) to ITRF given date and time of observation. How to convert coordinates from one of those two frames to horizontal azim...
orbital mechanics - How to convert TEME (or ITRF) to horizontal ...
I know that calculating the geocentric position of the respective Topos object at a specific time results in a Geocentric object that has an attribute .radec; however I am not confident that this delivers the right ascension in the TEME (Earth centered inertial frame.
The algorithm computes the positions (X, Y, Z) in the True Equator Mean Equinox coordinate frame (TEME). From that, I would like to find the corresponding RA DEC coordinates at the given epoch.