INTELSAT 4-F3
Satellite information INTELSAT 4-F3
| Spacetrack Directory Name | INTELSAT 4-F3 |
| Follow INTELSAT 4-F3 | INTELSAT 4-F3 Tracker |
| Pass predictions INTELSAT 4-F3 | Pass predictions INTELSAT 4-F3 |
| Orbit launches |
1971-12-20 (54 years ago)
|
| Days in orbit | 19987 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35916 km |
| Apogee | 36022 km |
| Orbit slope (inclination) | 6.2° |
| Laps per day | 1 |
| Height INTELSAT 4-F3 | 35968.36 km |
Additional information INTELSAT 4-F3
INTELSAT 4-F3, 5709 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Mon, 20 Dec 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-F3 Date of exalting 20.12.1971y. Average height of ISS INTELSAT 4-F3 hundred 35968.36 km. Average velocity INTELSAT 4-F3 is 11045.16 km/h. Inclination INTELSAT 4-F3 satellite 6.23°.TLE
Average velocity INTELSAT 4-F3
Average inclination INTELSAT 4-F3
Mean right ascension of the ascending node (RAAN) INTELSAT 4-F3
Mean argument of perigee INTELSAT 4-F3
Mean semi-major axis of the orbit INTELSAT 4-F3
Mean orbital eccentricity INTELSAT 4-F3
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