INTELSAT 602
Satellite information INTELSAT 602 - INTELSAT 602 (IS-602)
| Spacetrack Directory Name | INTELSAT 602 |
| Alternative name | INTELSAT 602 (IS-602) |
| Follow INTELSAT 602 | INTELSAT 602 Tracker |
| Pass predictions INTELSAT 602 | Pass predictions INTELSAT 602 |
| Orbit launches |
1989-10-27 (36 years ago)
|
| Days in orbit | 13477 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| WWW | Here |
| Perigee | 36143 km |
| Apogee | 36147 km |
| Orbit slope (inclination) | 14.37° |
| Laps per day | 1 |
| Height INTELSAT 602 | 36144.92 km |
Additional information INTELSAT 602
INTELSAT 602, 20315 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Fri, 27 Oct 1989 UTC via an ARIANE 44L launch vehicle from the French Guiana (FRGUI). 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 602 Date of exalting 27.10.1989y. Average height of ISS INTELSAT 602 hundred 36144.92 km. Average velocity INTELSAT 602 is 11022.27 km/h. Inclination INTELSAT 602 satellite 14.36°.TLE
Average velocity INTELSAT 602
Average inclination INTELSAT 602
Mean right ascension of the ascending node (RAAN) INTELSAT 602
Mean argument of perigee INTELSAT 602
Mean semi-major axis of the orbit INTELSAT 602
Mean orbital eccentricity INTELSAT 602
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