INTELSAT 3-F7
Satellite information INTELSAT 3-F7
| Spacetrack Directory Name | INTELSAT 3-F7 |
| Follow INTELSAT 3-F7 | INTELSAT 3-F7 Tracker |
| Pass predictions INTELSAT 3-F7 | Pass predictions INTELSAT 3-F7 |
| Orbit launches |
1970-04-23 (56 years ago)
|
| Days in orbit | 20593 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35770 km |
| Apogee | 35799 km |
| Orbit slope (inclination) | 2.64° |
| Laps per day | 1 |
| Height INTELSAT 3-F7 | 35781.66 km |
Additional information INTELSAT 3-F7
INTELSAT 3-F7, 4376 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Thu, 23 Apr 1970 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-F7 Date of exalting 23.04.1970y. Average height of ISS INTELSAT 3-F7 hundred 35781.66 km. Average velocity INTELSAT 3-F7 is 11069.56 km/h. Inclination INTELSAT 3-F7 satellite 2.6°.TLE
Average velocity INTELSAT 3-F7
Average inclination INTELSAT 3-F7
Mean right ascension of the ascending node (RAAN) INTELSAT 3-F7
Mean argument of perigee INTELSAT 3-F7
Mean semi-major axis of the orbit INTELSAT 3-F7
Mean orbital eccentricity INTELSAT 3-F7
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