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By adding the original line1 and line2 to TLE/TLEu object, users can use the original SGP4 predictor with sgp4 or orbit_predictor.
orbprop = orbit_predictor.sources.get_predictor_from_tle_lines(
(tle_obj.line1, tle_obj.line2))`
for x in range(100):
d = astropy.time.TimeDelta(x, format='sec')
t = epoch + d
print(t, orbprop_iridium106.propagate_eci(t.to_datetime()))
The text was updated successfully, but these errors were encountered:
tletools/tletools/tle.py
Line 169 in 6ccf12a
By adding the original line1 and line2 to TLE/TLEu object, users can use the original SGP4 predictor with sgp4 or orbit_predictor.
The text was updated successfully, but these errors were encountered: