INTELSAT 702
Satellite information INTELSAT 702 - INTELSAT 702 (IS-702)
| Spacetrack Directory Name | INTELSAT 702 |
| Alternative name | INTELSAT 702 (IS-702) |
| Follow INTELSAT 702 | INTELSAT 702 Tracker |
| Pass predictions INTELSAT 702 | Pass predictions INTELSAT 702 |
| Orbit launches |
1994-06-17 (32 years ago)
|
| Days in orbit | 11778 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Perigee | 36116 km |
| Apogee | 36214 km |
| Orbit slope (inclination) | 11.23° |
| Laps per day | 1 |
| Height INTELSAT 702 | 36164.26 km |
Additional information INTELSAT 702
INTELSAT 702, 23124 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Fri, 17 Jun 1994 UTC via an ARIANE 44LP 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 702 Date of exalting 17.06.1994y. Average height of ISS INTELSAT 702 hundred 36164.26 km. Average velocity INTELSAT 702 is 11019.7 km/h. Inclination INTELSAT 702 satellite 11.2°.TLE
Average velocity INTELSAT 702
Average inclination INTELSAT 702
Mean right ascension of the ascending node (RAAN) INTELSAT 702
Mean argument of perigee INTELSAT 702
Mean semi-major axis of the orbit INTELSAT 702
Mean orbital eccentricity INTELSAT 702
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