INTELSAT 504
Satellite information INTELSAT 504
| Spacetrack Directory Name | INTELSAT 504 |
| Follow INTELSAT 504 | INTELSAT 504 Tracker |
| Pass predictions INTELSAT 504 | Pass predictions INTELSAT 504 |
| Orbit launches |
1982-03-05 (44 years ago)
|
| Days in orbit | 16258 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36016 km |
| Apogee | 36149 km |
| Orbit slope (inclination) | 11.26° |
| Laps per day | 1 |
| Height INTELSAT 504 | 36083.36 km |
Additional information INTELSAT 504
INTELSAT 504, 13083 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Fri, 05 Mar 1982 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 504 Date of exalting 05.03.1982y. Average height of ISS INTELSAT 504 hundred 36083.36 km. Average velocity INTELSAT 504 is 11030.14 km/h. Inclination INTELSAT 504 satellite 11.28°.TLE
Average velocity INTELSAT 504
Average inclination INTELSAT 504
Mean right ascension of the ascending node (RAAN) INTELSAT 504
Mean argument of perigee INTELSAT 504
Mean semi-major axis of the orbit INTELSAT 504
Mean orbital eccentricity INTELSAT 504
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