INTELSAT 4-F7
Satellite information INTELSAT 4-F7
| Spacetrack Directory Name | INTELSAT 4-F7 |
| Follow INTELSAT 4-F7 | INTELSAT 4-F7 Tracker |
| Pass predictions INTELSAT 4-F7 | Pass predictions INTELSAT 4-F7 |
| Orbit launches |
1973-08-23 (53 years ago)
|
| Days in orbit | 19375 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36089 km |
| Apogee | 36123 km |
| Orbit slope (inclination) | 7.05° |
| Laps per day | 1 |
| Height INTELSAT 4-F7 | 36104.46 km |
Additional information INTELSAT 4-F7
INTELSAT 4-F7, 6796 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Thu, 23 Aug 1973 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-F7 Date of exalting 23.08.1973y. Average height of ISS INTELSAT 4-F7 hundred 36104.46 km. Average velocity INTELSAT 4-F7 is 11027.45 km/h. Inclination INTELSAT 4-F7 satellite 7.08°.TLE
Average velocity INTELSAT 4-F7
Average inclination INTELSAT 4-F7
Mean right ascension of the ascending node (RAAN) INTELSAT 4-F7
Mean argument of perigee INTELSAT 4-F7
Mean semi-major axis of the orbit INTELSAT 4-F7
Mean orbital eccentricity INTELSAT 4-F7
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