INTELSAT 605
Satellite information INTELSAT 605 - INTELSAT 605 (IS-605)
| Spacetrack Directory Name | INTELSAT 605 |
| Alternative name | INTELSAT 605 (IS-605) |
| Follow INTELSAT 605 | INTELSAT 605 Tracker |
| Pass predictions INTELSAT 605 | Pass predictions INTELSAT 605 |
| Orbit launches |
1991-08-14 (35 years ago)
|
| Days in orbit | 12821 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Perigee | 36045 km |
| Apogee | 36066 km |
| Orbit slope (inclination) | 13.67° |
| Laps per day | 1 |
| Height INTELSAT 605 | 36053.85 km |
Additional information INTELSAT 605
INTELSAT 605, 21653 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Wed, 14 Aug 1991 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 605 Date of exalting 14.08.1991y. Average height of ISS INTELSAT 605 hundred 36053.85 km. Average velocity INTELSAT 605 is 11034.06 km/h. Inclination INTELSAT 605 satellite 13.65°.TLE
Average velocity INTELSAT 605
Average inclination INTELSAT 605
Mean right ascension of the ascending node (RAAN) INTELSAT 605
Mean argument of perigee INTELSAT 605
Mean semi-major axis of the orbit INTELSAT 605
Mean orbital eccentricity INTELSAT 605
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