INTELSAT 4-F8
Satellite information INTELSAT 4-F8
| Spacetrack Directory Name | INTELSAT 4-F8 |
| Follow INTELSAT 4-F8 | INTELSAT 4-F8 Tracker |
| Pass predictions INTELSAT 4-F8 | Pass predictions INTELSAT 4-F8 |
| Orbit launches |
1974-11-21 (51 years ago)
|
| Days in orbit | 18920 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35908 km |
| Apogee | 35936 km |
| Orbit slope (inclination) | 7.8° |
| Laps per day | 1 |
| Height INTELSAT 4-F8 | 35922.86 km |
Additional information INTELSAT 4-F8
INTELSAT 4-F8, 7544 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Thu, 21 Nov 1974 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 4-F8 Date of exalting 21.11.1974y. Average height of ISS INTELSAT 4-F8 hundred 35922.86 km. Average velocity INTELSAT 4-F8 is 11051.09 km/h. Inclination INTELSAT 4-F8 satellite 7.83°.TLE
Average velocity INTELSAT 4-F8
Average inclination INTELSAT 4-F8
Mean right ascension of the ascending node (RAAN) INTELSAT 4-F8
Mean argument of perigee INTELSAT 4-F8
Mean semi-major axis of the orbit INTELSAT 4-F8
Mean orbital eccentricity INTELSAT 4-F8
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