INTELSAT 603
Satellite information INTELSAT 603 - INTELSAT 603 (IS-603)
| Spacetrack Directory Name | INTELSAT 603 |
| Alternative name | INTELSAT 603 (IS-603) |
| Follow INTELSAT 603 | INTELSAT 603 Tracker |
| Pass predictions INTELSAT 603 | Pass predictions INTELSAT 603 |
| Orbit launches |
1990-03-14 (36 years ago)
|
| Days in orbit | 13327 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35973 km |
| Apogee | 36047 km |
| Orbit slope (inclination) | 14.07° |
| Laps per day | 1 |
| Height INTELSAT 603 | 36011 km |
Additional information INTELSAT 603
INTELSAT 603, 20523 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Wed, 14 Mar 1990 UTC via a COMMERCIAL TITAN 3 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 603 Date of exalting 14.03.1990y. Average height of ISS INTELSAT 603 hundred 36011 km. Average velocity INTELSAT 603 is 11039.64 km/h. Inclination INTELSAT 603 satellite 14.06°.TLE
Average velocity INTELSAT 603
Average inclination INTELSAT 603
Mean right ascension of the ascending node (RAAN) INTELSAT 603
Mean argument of perigee INTELSAT 603
Mean semi-major axis of the orbit INTELSAT 603
Mean orbital eccentricity INTELSAT 603
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