INTELSAT 502
Satellite information INTELSAT 502
| Spacetrack Directory Name | INTELSAT 502 |
| Follow INTELSAT 502 | INTELSAT 502 Tracker |
| Pass predictions INTELSAT 502 | Pass predictions INTELSAT 502 |
| Orbit launches |
1980-12-06 (45 years ago)
|
| Days in orbit | 16712 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36125 km |
| Apogee | 36232 km |
| Orbit slope (inclination) | 11.18° |
| Laps per day | 1 |
| Height INTELSAT 502 | 36177.49 km |
Additional information INTELSAT 502
INTELSAT 502, 12089 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Sat, 06 Dec 1980 UTC via an ATLAS SLV-3D 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 502 Date of exalting 06.12.1980y. Average height of ISS INTELSAT 502 hundred 36177.49 km. Average velocity INTELSAT 502 is 11018.05 km/h. Inclination INTELSAT 502 satellite 11.2°.TLE
Average velocity INTELSAT 502
Average inclination INTELSAT 502
Mean right ascension of the ascending node (RAAN) INTELSAT 502
Mean argument of perigee INTELSAT 502
Mean semi-major axis of the orbit INTELSAT 502
Mean orbital eccentricity INTELSAT 502
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