HGS 1 (ASIASAT 3)
Satellite information HGS 1 (ASIASAT 3)
| Spacetrack Directory Name | HGS 1 (ASIASAT 3) |
| Follow HGS 1 (ASIASAT 3) | HGS 1 (ASIASAT 3) Tracker |
| Pass predictions HGS 1 (ASIASAT 3) | Pass predictions HGS 1 (ASIASAT 3) |
| Orbit launches |
1997-12-24 (28 years ago)
|
| Days in orbit | 10546 |
| Country/organisation of origin | USA (US) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 35585 km |
| Apogee | 36006 km |
| Orbit slope (inclination) | 13.39° |
| Laps per day | 1 |
| Height HGS 1 (ASIASAT 3) | 35794.33 km |
Additional information HGS 1 (ASIASAT 3)
HGS 1 (ASIASAT 3), 25126 is a payload satellite owned by Asiasat (US) in GEO that was launched on Wed, 24 Dec 1997 UTC via a PROTON-K/DM-2M launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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 HGS 1 (ASIASAT 3) Date of exalting 24.12.1997y. Average height of ISS HGS 1 (ASIASAT 3) hundred 35794.33 km. Average velocity HGS 1 (ASIASAT 3) is 11067.89 km/h. Inclination HGS 1 (ASIASAT 3) satellite 13.32°.TLE
Average velocity HGS 1 (ASIASAT 3)
Average inclination HGS 1 (ASIASAT 3)
Mean right ascension of the ascending node (RAAN) HGS 1 (ASIASAT 3)
Mean argument of perigee HGS 1 (ASIASAT 3)
Mean semi-major axis of the orbit HGS 1 (ASIASAT 3)
Mean orbital eccentricity HGS 1 (ASIASAT 3)
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