INTELSAT 3-F4
Satellite information INTELSAT 3-F4
| Spacetrack Directory Name | INTELSAT 3-F4 |
| Follow INTELSAT 3-F4 | INTELSAT 3-F4 Tracker |
| Pass predictions INTELSAT 3-F4 | Pass predictions INTELSAT 3-F4 |
| Orbit launches |
1969-05-22 (57 years ago)
|
| Days in orbit | 20930 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 38798 km |
| Apogee | 39045 km |
| Orbit slope (inclination) | 3.52° |
| Laps per day | 1 |
| Height INTELSAT 3-F4 | 38921.72 km |
Additional information INTELSAT 3-F4
INTELSAT 3-F4, 3947 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Thu, 22 May 1969 UTC via a THOR DELTA M 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 3-F4 Date of exalting 22.05.1969y. Average height of ISS INTELSAT 3-F4 hundred 38921.72 km. Average velocity INTELSAT 3-F4 is 10678.94 km/h. Inclination INTELSAT 3-F4 satellite 3.56°.TLE
Average velocity INTELSAT 3-F4
Average inclination INTELSAT 3-F4
Mean right ascension of the ascending node (RAAN) INTELSAT 3-F4
Mean argument of perigee INTELSAT 3-F4
Mean semi-major axis of the orbit INTELSAT 3-F4
Mean orbital eccentricity INTELSAT 3-F4
ISS
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