NAVSTAR 22 (USA 66)
Satellite information NAVSTAR 22 (USA 66) - GPS BIIA-10, SVN 23
| Spacetrack Directory Name | NAVSTAR 22 (USA 66) |
| Alternative name | GPS BIIA-10, SVN 23 |
| Follow NAVSTAR 22 (USA 66) | NAVSTAR 22 (USA 66) Tracker |
| Pass predictions NAVSTAR 22 (USA 66) | Pass predictions NAVSTAR 22 (USA 66) |
| Orbit launches |
1990-11-26 (35 years ago)
|
| Days in orbit | 13070 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 21287 km |
| Apogee | 21388 km |
| Orbit slope (inclination) | 56.25° |
| Laps per day | 2 |
| Height NAVSTAR 22 (USA 66) | 21344.71 km |
Additional information NAVSTAR 22 (USA 66)
NAVSTAR 22 (USA 66), 20959 is a payload satellite owned by USAF SSD (US) in MEO that was launched on Mon, 26 Nov 1990 UTC via a DELTA 7925 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 NAVSTAR 22 (USA 66) Date of exalting 26.11.1990y. Average height of ISS NAVSTAR 22 (USA 66) hundred 21344.71 km. Average velocity NAVSTAR 22 (USA 66) is 13652.49 km/h. Inclination NAVSTAR 22 (USA 66) satellite 56.25°.TLE
Average velocity NAVSTAR 22 (USA 66)
Average inclination NAVSTAR 22 (USA 66)
Mean right ascension of the ascending node (RAAN) NAVSTAR 22 (USA 66)
Mean argument of perigee NAVSTAR 22 (USA 66)
Mean semi-major axis of the orbit NAVSTAR 22 (USA 66)
Mean orbital eccentricity NAVSTAR 22 (USA 66)
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