INTELSAT 4-F5
Satellite information INTELSAT 4-F5
| Spacetrack Directory Name | INTELSAT 4-F5 |
| Follow INTELSAT 4-F5 | INTELSAT 4-F5 Tracker |
| Pass predictions INTELSAT 4-F5 | Pass predictions INTELSAT 4-F5 |
| Orbit launches |
1972-06-13 (54 years ago)
|
| Days in orbit | 19811 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35832 km |
| Apogee | 35842 km |
| Orbit slope (inclination) | 5.53° |
| Laps per day | 1 |
| Height INTELSAT 4-F5 | 35825.4 km |
Additional information INTELSAT 4-F5
INTELSAT 4-F5, 6052 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Tue, 13 Jun 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-F5 Date of exalting 13.06.1972y. Average height of ISS INTELSAT 4-F5 hundred 35825.4 km. Average velocity INTELSAT 4-F5 is 11063.83 km/h. Inclination INTELSAT 4-F5 satellite 5.57°.TLE
Average velocity INTELSAT 4-F5
Average inclination INTELSAT 4-F5
Mean right ascension of the ascending node (RAAN) INTELSAT 4-F5
Mean argument of perigee INTELSAT 4-F5
Mean semi-major axis of the orbit INTELSAT 4-F5
Mean orbital eccentricity INTELSAT 4-F5
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