INTELSAT 512
Satellite information INTELSAT 512
| Spacetrack Directory Name | INTELSAT 512 |
| Follow INTELSAT 512 | INTELSAT 512 Tracker |
| Pass predictions INTELSAT 512 | Pass predictions INTELSAT 512 |
| Orbit launches |
1985-09-28 (40 years ago)
|
| Days in orbit | 14955 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36074 km |
| Apogee | 36156 km |
| Orbit slope (inclination) | 14.05° |
| Laps per day | 1 |
| Height INTELSAT 512 | 36114.46 km |
Additional information INTELSAT 512
INTELSAT 512, 16101 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Sat, 28 Sep 1985 UTC via an ATLAS G CENTAUR 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 INTELSAT 512 Date of exalting 28.09.1985y. Average height of ISS INTELSAT 512 hundred 36114.46 km. Average velocity INTELSAT 512 is 11026.19 km/h. Inclination INTELSAT 512 satellite 14.05°.TLE
Average velocity INTELSAT 512
Average inclination INTELSAT 512
Mean right ascension of the ascending node (RAAN) INTELSAT 512
Mean argument of perigee INTELSAT 512
Mean semi-major axis of the orbit INTELSAT 512
Mean orbital eccentricity INTELSAT 512
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