INTELSAT 3-F8
Satellite information INTELSAT 3-F8
| Spacetrack Directory Name | INTELSAT 3-F8 |
| Follow INTELSAT 3-F8 | INTELSAT 3-F8 Tracker |
| Pass predictions INTELSAT 3-F8 | Pass predictions INTELSAT 3-F8 |
| Orbit launches |
1970-07-23 (56 years ago)
|
| Days in orbit | 20502 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 33871 km |
| Apogee | 36604 km |
| Orbit slope (inclination) | 5.66° |
| Laps per day | 1 |
| Height INTELSAT 3-F8 | 35264.96 km |
Additional information INTELSAT 3-F8
INTELSAT 3-F8, 4478 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Thu, 23 Jul 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-F8 Date of exalting 23.07.1970y. Average height of ISS INTELSAT 3-F8 hundred 35264.96 km. Average velocity INTELSAT 3-F8 is 11137.1 km/h. Inclination INTELSAT 3-F8 satellite 5.63°.TLE
Average velocity INTELSAT 3-F8
Average inclination INTELSAT 3-F8
Mean right ascension of the ascending node (RAAN) INTELSAT 3-F8
Mean argument of perigee INTELSAT 3-F8
Mean semi-major axis of the orbit INTELSAT 3-F8
Mean orbital eccentricity INTELSAT 3-F8
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