INTELSAT 510
Satellite information INTELSAT 510
| Spacetrack Directory Name | INTELSAT 510 |
| Follow INTELSAT 510 | INTELSAT 510 Tracker |
| Pass predictions INTELSAT 510 | Pass predictions INTELSAT 510 |
| Orbit launches |
1985-03-22 (41 years ago)
|
| Days in orbit | 15145 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36205 km |
| Apogee | 36503 km |
| Orbit slope (inclination) | 13.69° |
| Laps per day | 1 |
| Height INTELSAT 510 | 36354.92 km |
Additional information INTELSAT 510
INTELSAT 510, 15629 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Fri, 22 Mar 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 510 Date of exalting 22.03.1985y. Average height of ISS INTELSAT 510 hundred 36354.92 km. Average velocity INTELSAT 510 is 10995.04 km/h. Inclination INTELSAT 510 satellite 13.7°.TLE
Average velocity INTELSAT 510
Average inclination INTELSAT 510
Mean right ascension of the ascending node (RAAN) INTELSAT 510
Mean argument of perigee INTELSAT 510
Mean semi-major axis of the orbit INTELSAT 510
Mean orbital eccentricity INTELSAT 510
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