A-1 (ASTERIX)
Satellite information A-1 (ASTERIX)
| Spacetrack Directory Name | A-1 (ASTERIX) |
| Follow A-1 (ASTERIX) | A-1 (ASTERIX) Tracker |
| Pass predictions A-1 (ASTERIX) | Pass predictions A-1 (ASTERIX) |
| Orbit launches |
1965-11-26 (60 years ago)
|
| Days in orbit | 22181 |
| Country/organisation of origin | Francja (FR) |
| Starting point | HGSTR (Hammaguir Launch Site, Algeria) |
| Perigee | 523 km |
| Apogee | 1644 km |
| Orbit slope (inclination) | 34.26° |
| Laps per day | 14 |
| Height A-1 (ASTERIX) | 1092.96 km |
Additional information A-1 (ASTERIX)
A-1 (ASTERIX), 1778 is a payload satellite owned by CNES (FR) in LEO that was launched on Fri, 26 Nov 1965 UTC via a DIAMANT A launch vehicle from the Hamma Guira Space Track Range (HGSTR). 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 A-1 (ASTERIX) Date of exalting 26.11.1965y. Average height of ISS A-1 (ASTERIX) hundred 1092.96 km. Average velocity A-1 (ASTERIX) is 26312.37 km/h. Inclination A-1 (ASTERIX) satellite 34.26°.TLE
Average velocity A-1 (ASTERIX)
Average inclination A-1 (ASTERIX)
Mean right ascension of the ascending node (RAAN) A-1 (ASTERIX)
Mean argument of perigee A-1 (ASTERIX)
Mean semi-major axis of the orbit A-1 (ASTERIX)
Mean orbital eccentricity A-1 (ASTERIX)
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