INTELSAT 4-F4
Satellite information INTELSAT 4-F4
| Spacetrack Directory Name | INTELSAT 4-F4 |
| Follow INTELSAT 4-F4 | INTELSAT 4-F4 Tracker |
| Pass predictions INTELSAT 4-F4 | Pass predictions INTELSAT 4-F4 |
| Orbit launches |
1972-01-23 (54 years ago)
|
| Days in orbit | 19953 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35896 km |
| Apogee | 35930 km |
| Orbit slope (inclination) | 6.55° |
| Laps per day | 1 |
| Height INTELSAT 4-F4 | 35911.6 km |
Additional information INTELSAT 4-F4
INTELSAT 4-F4, 5775 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Sun, 23 Jan 1972 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-F4 Date of exalting 23.01.1972y. Average height of ISS INTELSAT 4-F4 hundred 35911.6 km. Average velocity INTELSAT 4-F4 is 11052.56 km/h. Inclination INTELSAT 4-F4 satellite 6.59°.TLE
Average velocity INTELSAT 4-F4
Average inclination INTELSAT 4-F4
Mean right ascension of the ascending node (RAAN) INTELSAT 4-F4
Mean argument of perigee INTELSAT 4-F4
Mean semi-major axis of the orbit INTELSAT 4-F4
Mean orbital eccentricity INTELSAT 4-F4
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