INTELSAT 704
Satellite information INTELSAT 704 - INTELSAT 704 (IS-704)
| Spacetrack Directory Name | INTELSAT 704 |
| Alternative name | INTELSAT 704 (IS-704) |
| Follow INTELSAT 704 | INTELSAT 704 Tracker |
| Pass predictions INTELSAT 704 | Pass predictions INTELSAT 704 |
| Orbit launches |
1995-01-10 (31 years ago)
|
| Days in orbit | 11563 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36087 km |
| Apogee | 36103 km |
| Orbit slope (inclination) | 12° |
| Laps per day | 1 |
| Height INTELSAT 704 | 36094.62 km |
Additional information INTELSAT 704
INTELSAT 704, 23461 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Tue, 10 Jan 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 704 Date of exalting 10.01.1995y. Average height of ISS INTELSAT 704 hundred 36094.62 km. Average velocity INTELSAT 704 is 11028.76 km/h. Inclination INTELSAT 704 satellite 11.98°.TLE
Average velocity INTELSAT 704
Average inclination INTELSAT 704
Mean right ascension of the ascending node (RAAN) INTELSAT 704
Mean argument of perigee INTELSAT 704
Mean semi-major axis of the orbit INTELSAT 704
Mean orbital eccentricity INTELSAT 704
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