I am still very new to all things Cesium and astrodynamics so forgive my ignorance.
I am using a TLE propagator to show the ISS on the Cesium globe to help build an analytical tool for Space. The TLE propagator returns predictions in TEME. I was hoping to create a Cesium.Cartesian3 point by calling something like
which I don’t think exists.
Like others, I did find
but I don’t understand how to use it for my purposes.
Any guidance with converting TEME ECI to lat/long/deg, such that I could use it as a position in an Entity, would be much appreciated.