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I'm writing my own library for making life easier when working with orbits.
Your readme indicates that your library can be used to convert between reference frames which is great because I need the ability to convert between J2000, SGP4 TEME, and ICRF.
However, I can't seem to work out how to do this with your library. Am I missing something here?
The text was updated successfully, but these errors were encountered:
Apologies for the delay. SGP.NET emits a TEME ECI from Sgp4::FindPosition, and, by extension, all ECI coordinates referenced within SGP.NET are TEME. It does not support J2000 or ICRF ECI coordinate systems, although Skyfield for Python does, which might be of some help if you want to implement the conversion equations.
When referring to reference frames in the README, I had things like ground station observations in mind. I'm sorry I couldn't be of more help, I just haven't had the motivation to implement it for my use cases.
I'm writing my own library for making life easier when working with orbits.
Your readme indicates that your library can be used to convert between reference frames which is great because I need the ability to convert between
J2000
,SGP4 TEME
, andICRF
.However, I can't seem to work out how to do this with your library. Am I missing something here?
The text was updated successfully, but these errors were encountered: