NAVSTAR 26 (USA 83)
Satellite information NAVSTAR 26 (USA 83) - GPS BIIA-14, SVN 26
| Spacetrack Directory Name | NAVSTAR 26 (USA 83) |
| Alternative name | GPS BIIA-14, SVN 26 |
| Follow NAVSTAR 26 (USA 83) | NAVSTAR 26 (USA 83) Tracker |
| Pass predictions NAVSTAR 26 (USA 83) | Pass predictions NAVSTAR 26 (USA 83) |
| Orbit launches |
1992-07-07 (34 years ago)
|
| Days in orbit | 12481 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 21352 km |
| Apogee | 21371 km |
| Orbit slope (inclination) | 55.55° |
| Laps per day | 2 |
| Height NAVSTAR 26 (USA 83) | 21368.73 km |
Additional information NAVSTAR 26 (USA 83)
NAVSTAR 26 (USA 83), 22014 is a payload satellite owned by USAF SMC (US) in MEO that was launched on Tue, 07 Jul 1992 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 26 (USA 83) Date of exalting 07.07.1992y. Average height of ISS NAVSTAR 26 (USA 83) hundred 21368.73 km. Average velocity NAVSTAR 26 (USA 83) is 13646.49 km/h. Inclination NAVSTAR 26 (USA 83) satellite 55.55°.TLE
Average velocity NAVSTAR 26 (USA 83)
Average inclination NAVSTAR 26 (USA 83)
Mean right ascension of the ascending node (RAAN) NAVSTAR 26 (USA 83)
Mean argument of perigee NAVSTAR 26 (USA 83)
Mean semi-major axis of the orbit NAVSTAR 26 (USA 83)
Mean orbital eccentricity NAVSTAR 26 (USA 83)
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