INTELSAT 2-F1
Satellite information INTELSAT 2-F1
| Spacetrack Directory Name | INTELSAT 2-F1 |
| Follow INTELSAT 2-F1 | INTELSAT 2-F1 Tracker |
| Pass predictions INTELSAT 2-F1 | Pass predictions INTELSAT 2-F1 |
| Orbit launches |
1966-10-26 (59 years ago)
|
| Days in orbit | 21869 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 3193 km |
| Apogee | 37180 km |
| Orbit slope (inclination) | 18.3° |
| Laps per day | 2 |
| Height INTELSAT 2-F1 | 25605.48 km |
Additional information INTELSAT 2-F1
INTELSAT 2-F1, 2514 is a payload satellite owned by INTELSAT (US) in HEO that was launched on Wed, 26 Oct 1966 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-F1 Date of exalting 26.10.1966y. Average height of ISS INTELSAT 2-F1 hundred 25605.48 km. Average velocity INTELSAT 2-F1 is 12388.93 km/h. Inclination INTELSAT 2-F1 satellite 18.25°.TLE
Average velocity INTELSAT 2-F1
Average inclination INTELSAT 2-F1
Mean right ascension of the ascending node (RAAN) INTELSAT 2-F1
Mean argument of perigee INTELSAT 2-F1
Mean semi-major axis of the orbit INTELSAT 2-F1
Mean orbital eccentricity INTELSAT 2-F1
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