INTELSAT 4-F2
Satellite information INTELSAT 4-F2
| Spacetrack Directory Name | INTELSAT 4-F2 |
| Follow INTELSAT 4-F2 | INTELSAT 4-F2 Tracker |
| Pass predictions INTELSAT 4-F2 | Pass predictions INTELSAT 4-F2 |
| Orbit launches |
1971-01-26 (55 years ago)
|
| Days in orbit | 20315 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36130 km |
| Apogee | 36256 km |
| Orbit slope (inclination) | 4.13° |
| Laps per day | 1 |
| Height INTELSAT 4-F2 | 36193.64 km |
Additional information INTELSAT 4-F2
INTELSAT 4-F2, 4881 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Tue, 26 Jan 1971 UTC via an ATLAS SLV-3C 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 4-F2 Date of exalting 26.01.1971y. Average height of ISS INTELSAT 4-F2 hundred 36193.64 km. Average velocity INTELSAT 4-F2 is 11015.81 km/h. Inclination INTELSAT 4-F2 satellite 4.17°.TLE
Average velocity INTELSAT 4-F2
Average inclination INTELSAT 4-F2
Mean right ascension of the ascending node (RAAN) INTELSAT 4-F2
Mean argument of perigee INTELSAT 4-F2
Mean semi-major axis of the orbit INTELSAT 4-F2
Mean orbital eccentricity INTELSAT 4-F2
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