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Derive mean_motion_derivative (ndot) and mean_motion_sec_derivative (nddot) if not available from TLE.
https://github.com/consensys-space/trusat-orbit/blob/00bf2f2a9f674e03e4b01fbc73fb1bb48e6df494/tle_util.py#L422
SGP4 units: satrec.ndot = satrec.ndot / (xpdotp1440.0); satrec.nddot= satrec.nddot / (xpdotp1440.0*1440);
The text was updated successfully, but these errors were encountered:
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Derive mean_motion_derivative (ndot) and mean_motion_sec_derivative (nddot) if not available from TLE.
https://github.com/consensys-space/trusat-orbit/blob/00bf2f2a9f674e03e4b01fbc73fb1bb48e6df494/tle_util.py#L422
SGP4 units:
satrec.ndot = satrec.ndot / (xpdotp1440.0);
satrec.nddot= satrec.nddot / (xpdotp1440.0*1440);
The text was updated successfully, but these errors were encountered: