NAVSTAR 30 (USA 88)
Satellite information NAVSTAR 30 (USA 88) - GPS BIIA-18, SVN 22
| Spacetrack Directory Name | NAVSTAR 30 (USA 88) |
| Alternative name | GPS BIIA-18, SVN 22 |
| Follow NAVSTAR 30 (USA 88) | NAVSTAR 30 (USA 88) Tracker |
| Pass predictions NAVSTAR 30 (USA 88) | Pass predictions NAVSTAR 30 (USA 88) |
| Orbit launches |
1993-02-03 (33 years ago)
|
| Days in orbit | 12270 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 21276 km |
| Apogee | 21411 km |
| Orbit slope (inclination) | 53.23° |
| Laps per day | 2 |
| Height NAVSTAR 30 (USA 88) | 21350.55 km |
Additional information NAVSTAR 30 (USA 88)
NAVSTAR 30 (USA 88), 22446 is a payload satellite owned by USAF SMC (US) in MEO that was launched on Wed, 03 Feb 1993 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 30 (USA 88) Date of exalting 03.02.1993y. Average height of ISS NAVSTAR 30 (USA 88) hundred 21350.55 km. Average velocity NAVSTAR 30 (USA 88) is 13650.86 km/h. Inclination NAVSTAR 30 (USA 88) satellite 53.24°.TLE
Average velocity NAVSTAR 30 (USA 88)
Average inclination NAVSTAR 30 (USA 88)
Mean right ascension of the ascending node (RAAN) NAVSTAR 30 (USA 88)
Mean argument of perigee NAVSTAR 30 (USA 88)
Mean semi-major axis of the orbit NAVSTAR 30 (USA 88)
Mean orbital eccentricity NAVSTAR 30 (USA 88)
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