INTELSAT 506
Satellite information INTELSAT 506
| Spacetrack Directory Name | INTELSAT 506 |
| Follow INTELSAT 506 | INTELSAT 506 Tracker |
| Pass predictions INTELSAT 506 | Pass predictions INTELSAT 506 |
| Orbit launches |
1983-05-19 (43 years ago)
|
| Days in orbit | 15818 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35929 km |
| Apogee | 36271 km |
| Orbit slope (inclination) | 12.38° |
| Laps per day | 1 |
| Height INTELSAT 506 | 36101.66 km |
Additional information INTELSAT 506
INTELSAT 506, 14077 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Thu, 19 May 1983 UTC via an ATLAS SLV-3D CENTAUR 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 506 Date of exalting 19.05.1983y. Average height of ISS INTELSAT 506 hundred 36101.66 km. Average velocity INTELSAT 506 is 11027.76 km/h. Inclination INTELSAT 506 satellite 12.39°.TLE
Average velocity INTELSAT 506
Average inclination INTELSAT 506
Mean right ascension of the ascending node (RAAN) INTELSAT 506
Mean argument of perigee INTELSAT 506
Mean semi-major axis of the orbit INTELSAT 506
Mean orbital eccentricity INTELSAT 506
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