INTELSAT 4A-F1
Satellite information INTELSAT 4A-F1
| Spacetrack Directory Name | INTELSAT 4A-F1 |
| Follow INTELSAT 4A-F1 | INTELSAT 4A-F1 Tracker |
| Pass predictions INTELSAT 4A-F1 | Pass predictions INTELSAT 4A-F1 |
| Orbit launches |
1975-09-26 (50 years ago)
|
| Days in orbit | 18611 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35874 km |
| Apogee | 35895 km |
| Orbit slope (inclination) | 7.7° |
| Laps per day | 1 |
| Height INTELSAT 4A-F1 | 35885.13 km |
Additional information INTELSAT 4A-F1
INTELSAT 4A-F1, 8330 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Fri, 26 Sep 1975 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-F1 Date of exalting 26.09.1975y. Average height of ISS INTELSAT 4A-F1 hundred 35885.13 km. Average velocity INTELSAT 4A-F1 is 11056.02 km/h. Inclination INTELSAT 4A-F1 satellite 7.73°.TLE
Average velocity INTELSAT 4A-F1
Average inclination INTELSAT 4A-F1
Mean right ascension of the ascending node (RAAN) INTELSAT 4A-F1
Mean argument of perigee INTELSAT 4A-F1
Mean semi-major axis of the orbit INTELSAT 4A-F1
Mean orbital eccentricity INTELSAT 4A-F1
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