INTELSAT 2-F3
Satellite information INTELSAT 2-F3
| Spacetrack Directory Name | INTELSAT 2-F3 |
| Follow INTELSAT 2-F3 | INTELSAT 2-F3 Tracker |
| Pass predictions INTELSAT 2-F3 | Pass predictions INTELSAT 2-F3 |
| Orbit launches |
1967-03-23 (59 years ago)
|
| Days in orbit | 21721 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| WWW | Here |
| Perigee | 35701 km |
| Apogee | 35869 km |
| Orbit slope (inclination) | 4.28° |
| Laps per day | 1 |
| Height INTELSAT 2-F3 | 35754.44 km |
Additional information INTELSAT 2-F3
INTELSAT 2-F3, 2717 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Thu, 23 Mar 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-F3 Date of exalting 23.03.1967y. Average height of ISS INTELSAT 2-F3 hundred 35754.44 km. Average velocity INTELSAT 2-F3 is 11073.16 km/h. Inclination INTELSAT 2-F3 satellite 4.25°.TLE
Average velocity INTELSAT 2-F3
Average inclination INTELSAT 2-F3
Mean right ascension of the ascending node (RAAN) INTELSAT 2-F3
Mean argument of perigee INTELSAT 2-F3
Mean semi-major axis of the orbit INTELSAT 2-F3
Mean orbital eccentricity INTELSAT 2-F3
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