SATCOM C4
Satellite information SATCOM C4
| Spacetrack Directory Name | SATCOM C4 |
| Follow SATCOM C4 | SATCOM C4 Tracker |
| Pass predictions SATCOM C4 | Pass predictions SATCOM C4 |
| Orbit launches |
1992-08-31 (34 years ago)
|
| Days in orbit | 12426 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36123 km |
| Apogee | 36160 km |
| Orbit slope (inclination) | 13.83° |
| Laps per day | 1 |
| Height SATCOM C4 | 36141.92 km |
Additional information SATCOM C4
SATCOM C4, 22096 is a payload satellite owned by GE Americom (US) in GEO that was launched on Mon, 31 Aug 1992 UTC via a DELTA 7925 launch vehicle from the Air Force Eastern Test Range (AFETR). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
satellite SATCOM C4 Date of exalting 31.08.1992y. Average height of ISS SATCOM C4 hundred 36141.92 km. Average velocity SATCOM C4 is 11022.64 km/h. Inclination SATCOM C4 satellite 13.82°.TLE
Average velocity SATCOM C4
Average inclination SATCOM C4
Mean right ascension of the ascending node (RAAN) SATCOM C4
Mean argument of perigee SATCOM C4
Mean semi-major axis of the orbit SATCOM C4
Mean orbital eccentricity SATCOM C4
ISS
Buy us a coffee!
