INTELSAT 3-F2
Satellite information INTELSAT 3-F2
| Spacetrack Directory Name | INTELSAT 3-F2 |
| Follow INTELSAT 3-F2 | INTELSAT 3-F2 Tracker |
| Pass predictions INTELSAT 3-F2 | Pass predictions INTELSAT 3-F2 |
| Orbit launches |
1968-12-19 (57 years ago)
|
| Days in orbit | 21127 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 38434 km |
| Apogee | 39309 km |
| Orbit slope (inclination) | 3.71° |
| Laps per day | 1 |
| Height INTELSAT 3-F2 | 38873.29 km |
Additional information INTELSAT 3-F2
INTELSAT 3-F2, 3623 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Thu, 19 Dec 1968 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-F2 Date of exalting 19.12.1968y. Average height of ISS INTELSAT 3-F2 hundred 38873.29 km. Average velocity INTELSAT 3-F2 is 10684.67 km/h. Inclination INTELSAT 3-F2 satellite 3.8°.TLE
Average velocity INTELSAT 3-F2
Average inclination INTELSAT 3-F2
Mean right ascension of the ascending node (RAAN) INTELSAT 3-F2
Mean argument of perigee INTELSAT 3-F2
Mean semi-major axis of the orbit INTELSAT 3-F2
Mean orbital eccentricity INTELSAT 3-F2
ISS
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