I'm evaluating the use of skyfield for an application to earth observation satellites, I understand this is not a target use case at the moment, but I easily managed to extract the satellite orbital mechanics out of EarthSatellite with a modicum of code duplication, so I'd like to know if you are interested in supporting some basic form of this use case.
As an example the EarthSatellite class compute the ITRF position of the satellite for a given time object inside _compute_GCRS, but doesn't expose it in the API:
I'm evaluating the use of skyfield for an application to earth observation satellites, I understand this is not a target use case at the moment, but I easily managed to extract the satellite orbital mechanics out of
EarthSatellite
with a modicum of code duplication, so I'd like to know if you are interested in supporting some basic form of this use case.As an example the
EarthSatellite
class compute the ITRF position of the satellite for a given time object inside_compute_GCRS
, but doesn't expose it in the API:https://github.com/skyfielders/python-skyfield/blob/master/skyfield/sgp4lib.py#L67
Could you please add a
EarthSatellite.itrf
method that returns therITRF
andvITRF
quantities already computed?