INTELSAT 709
Satellite information INTELSAT 709 - INTELSAT 709 (IS-709)
| Spacetrack Directory Name | INTELSAT 709 |
| Alternative name | INTELSAT 709 (IS-709) |
| Follow INTELSAT 709 | INTELSAT 709 Tracker |
| Pass predictions INTELSAT 709 | Pass predictions INTELSAT 709 |
| Orbit launches |
1996-06-15 (30 years ago)
|
| Days in orbit | 11048 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Perigee | 36034 km |
| Apogee | 36158 km |
| Orbit slope (inclination) | 10.92° |
| Laps per day | 1 |
| Height INTELSAT 709 | 36095.52 km |
Additional information INTELSAT 709
INTELSAT 709, 23915 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Sat, 15 Jun 1996 UTC via an ARIANE 44P 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 709 Date of exalting 15.06.1996y. Average height of ISS INTELSAT 709 hundred 36095.52 km. Average velocity INTELSAT 709 is 11028.56 km/h. Inclination INTELSAT 709 satellite 10.89°.TLE
Average velocity INTELSAT 709
Average inclination INTELSAT 709
Mean right ascension of the ascending node (RAAN) INTELSAT 709
Mean argument of perigee INTELSAT 709
Mean semi-major axis of the orbit INTELSAT 709
Mean orbital eccentricity INTELSAT 709
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