AMOS 5I (ASIASAT 2)
Satellite information AMOS 5I (ASIASAT 2) - ASIASAT 2
| Spacetrack Directory Name | AMOS 5I (ASIASAT 2) |
| Alternative name | ASIASAT 2 |
| Follow AMOS 5I (ASIASAT 2) | AMOS 5I (ASIASAT 2) Tracker |
| Pass predictions AMOS 5I (ASIASAT 2) | Pass predictions AMOS 5I (ASIASAT 2) |
| Orbit launches |
1995-11-28 (30 years ago)
|
| Days in orbit | 11248 |
| Country/organisation of origin | Izrael (ISRA) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Perigee | 36010 km |
| Apogee | 36108 km |
| Orbit slope (inclination) | 11.46° |
| Laps per day | 1 |
| Height AMOS 5I (ASIASAT 2) | 36059.54 km |
Additional information AMOS 5I (ASIASAT 2)
AMOS 5I (ASIASAT 2), 23723 is a payload satellite owned by Asiasat (IL) in GEO that was launched on Tue, 28 Nov 1995 UTC via a CHANG ZHENG 2E launch vehicle from the Xichang Space Center, China (XSC). 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 AMOS 5I (ASIASAT 2) Date of exalting 28.11.1995y. Average height of ISS AMOS 5I (ASIASAT 2) hundred 36059.54 km. Average velocity AMOS 5I (ASIASAT 2) is 11033.29 km/h. Inclination AMOS 5I (ASIASAT 2) satellite 11.43°.TLE
Average velocity AMOS 5I (ASIASAT 2)
Average inclination AMOS 5I (ASIASAT 2)
Mean right ascension of the ascending node (RAAN) AMOS 5I (ASIASAT 2)
Mean argument of perigee AMOS 5I (ASIASAT 2)
Mean semi-major axis of the orbit AMOS 5I (ASIASAT 2)
Mean orbital eccentricity AMOS 5I (ASIASAT 2)
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