NAVSTAR 25 (USA 80)
Satellite information NAVSTAR 25 (USA 80) - GPS BIIA-13, SVN 28
| Spacetrack Directory Name | NAVSTAR 25 (USA 80) |
| Alternative name | GPS BIIA-13, SVN 28 |
| Follow NAVSTAR 25 (USA 80) | NAVSTAR 25 (USA 80) Tracker |
| Pass predictions NAVSTAR 25 (USA 80) | Pass predictions NAVSTAR 25 (USA 80) |
| Orbit launches |
1992-04-10 (34 years ago)
|
| Days in orbit | 12569 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 21297 km |
| Apogee | 21476 km |
| Orbit slope (inclination) | 54.87° |
| Laps per day | 2 |
| Height NAVSTAR 25 (USA 80) | 21393.28 km |
Additional information NAVSTAR 25 (USA 80)
NAVSTAR 25 (USA 80), 21930 is a payload satellite owned by USAF SSD (US) in MEO that was launched on Fri, 10 Apr 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 25 (USA 80) Date of exalting 10.04.1992y. Average height of ISS NAVSTAR 25 (USA 80) hundred 21393.28 km. Average velocity NAVSTAR 25 (USA 80) is 13640.45 km/h. Inclination NAVSTAR 25 (USA 80) satellite 54.88°.TLE
Average velocity NAVSTAR 25 (USA 80)
Average inclination NAVSTAR 25 (USA 80)
Mean right ascension of the ascending node (RAAN) NAVSTAR 25 (USA 80)
Mean argument of perigee NAVSTAR 25 (USA 80)
Mean semi-major axis of the orbit NAVSTAR 25 (USA 80)
Mean orbital eccentricity NAVSTAR 25 (USA 80)
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