INTELSAT 4A-F6
Satellite information INTELSAT 4A-F6
| Spacetrack Directory Name | INTELSAT 4A-F6 |
| Follow INTELSAT 4A-F6 | INTELSAT 4A-F6 Tracker |
| Pass predictions INTELSAT 4A-F6 | Pass predictions INTELSAT 4A-F6 |
| Orbit launches |
1978-03-31 (48 years ago)
|
| Days in orbit | 17694 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35754 km |
| Apogee | 35799 km |
| Orbit slope (inclination) | 8.62° |
| Laps per day | 1 |
| Height INTELSAT 4A-F6 | 35798.45 km |
Additional information INTELSAT 4A-F6
INTELSAT 4A-F6, 10778 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Fri, 31 Mar 1978 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 4A-F6 Date of exalting 31.03.1978y. Average height of ISS INTELSAT 4A-F6 hundred 35798.45 km. Average velocity INTELSAT 4A-F6 is 11067.37 km/h. Inclination INTELSAT 4A-F6 satellite 8.64°.TLE
Average velocity INTELSAT 4A-F6
Average inclination INTELSAT 4A-F6
Mean right ascension of the ascending node (RAAN) INTELSAT 4A-F6
Mean argument of perigee INTELSAT 4A-F6
Mean semi-major axis of the orbit INTELSAT 4A-F6
Mean orbital eccentricity INTELSAT 4A-F6
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