https://au.mathworks.com/help/satcom/gs/satelliteScenario-key-conc
- Coordinate Systems
- Geodetic coordinates – (lat, lon, h); lattitude, longitude, ellipsoidal height
- Earth Centered Earth-Fixed Coordinates
- …
- Orbital Elements
- Eccentricity (e)
- Semimajor Axis (a)
- Inclination (i)
- Right ascension of ascending node (Ω) – RAAN
- Argument of periapsis (ω)
- True Anomaly (v)
- Two Line Element (TLE) Files
- Data format encoding list of orbital elements at a given point in time
- Consists of 3 lines
- Satellite 1
- 1 -42U 20042A 20154.78005548 .00000000 00000-0 10000-3 0 15
- 2 -42 55.0000 175.0000 0010000 100.0000 174.9900 12.60262048 485
- https://www.space-track.org/documentation#tle
https://au.mathworks.com/help/satcom/ug/satellite-constellation-access-to-groundstation.html