INTELSAT 705
Satellite information INTELSAT 705 - INTELSAT 705 (IS-705)
| Spacetrack Directory Name | INTELSAT 705 |
| Alternative name | INTELSAT 705 (IS-705) |
| Follow INTELSAT 705 | INTELSAT 705 Tracker |
| Pass predictions INTELSAT 705 | Pass predictions INTELSAT 705 |
| Orbit launches |
1995-03-22 (31 years ago)
|
| Days in orbit | 11492 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36080 km |
| Apogee | 36228 km |
| Orbit slope (inclination) | 11.86° |
| Laps per day | 1 |
| Height INTELSAT 705 | 36153.7 km |
Additional information INTELSAT 705
INTELSAT 705, 23528 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Wed, 22 Mar 1995 UTC via an ATLAS IIAS 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 705 Date of exalting 22.03.1995y. Average height of ISS INTELSAT 705 hundred 36153.7 km. Average velocity INTELSAT 705 is 11021.18 km/h. Inclination INTELSAT 705 satellite 11.84°.TLE
Average velocity INTELSAT 705
Average inclination INTELSAT 705
Mean right ascension of the ascending node (RAAN) INTELSAT 705
Mean argument of perigee INTELSAT 705
Mean semi-major axis of the orbit INTELSAT 705
Mean orbital eccentricity INTELSAT 705
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