INTELSAT 1-F1
Satellite information INTELSAT 1-F1 - EARLY BIRD
| Spacetrack Directory Name | INTELSAT 1-F1 |
| Alternative name | EARLY BIRD |
| Follow INTELSAT 1-F1 | INTELSAT 1-F1 Tracker |
| Pass predictions INTELSAT 1-F1 | Pass predictions INTELSAT 1-F1 |
| Orbit launches |
1965-04-06 (61 years ago)
|
| Days in orbit | 22438 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35770 km |
| Apogee | 35795 km |
| Orbit slope (inclination) | 7.36° |
| Laps per day | 1 |
| Height INTELSAT 1-F1 | 35803.54 km |
Additional information INTELSAT 1-F1
INTELSAT 1-F1, 1317 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Tue, 06 Apr 1965 UTC via a THOR DELTA D 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 1-F1 Date of exalting 06.04.1965y. Average height of ISS INTELSAT 1-F1 hundred 35803.54 km. Average velocity INTELSAT 1-F1 is 11066.71 km/h. Inclination INTELSAT 1-F1 satellite 7.32°.TLE
Average velocity INTELSAT 1-F1
Average inclination INTELSAT 1-F1
Mean right ascension of the ascending node (RAAN) INTELSAT 1-F1
Mean argument of perigee INTELSAT 1-F1
Mean semi-major axis of the orbit INTELSAT 1-F1
Mean orbital eccentricity INTELSAT 1-F1
ISS
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