INTELSAT 2-F4
Satellite information INTELSAT 2-F4
| Spacetrack Directory Name | INTELSAT 2-F4 |
| Follow INTELSAT 2-F4 | INTELSAT 2-F4 Tracker |
| Pass predictions INTELSAT 2-F4 | Pass predictions INTELSAT 2-F4 |
| Orbit launches |
1967-09-28 (58 years ago)
|
| Days in orbit | 21532 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35768 km |
| Apogee | 35866 km |
| Orbit slope (inclination) | 4.28° |
| Laps per day | 1 |
| Height INTELSAT 2-F4 | 35766.93 km |
Additional information INTELSAT 2-F4
INTELSAT 2-F4, 2969 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Thu, 28 Sep 1967 UTC via a THOR DELTA E1 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 2-F4 Date of exalting 28.09.1967y. Average height of ISS INTELSAT 2-F4 hundred 35766.93 km. Average velocity INTELSAT 2-F4 is 11071.52 km/h. Inclination INTELSAT 2-F4 satellite 4.25°.TLE
Average velocity INTELSAT 2-F4
Average inclination INTELSAT 2-F4
Mean right ascension of the ascending node (RAAN) INTELSAT 2-F4
Mean argument of perigee INTELSAT 2-F4
Mean semi-major axis of the orbit INTELSAT 2-F4
Mean orbital eccentricity INTELSAT 2-F4
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