NATO 4B
Satellite information NATO 4B
| Spacetrack Directory Name | NATO 4B |
| Follow NATO 4B | NATO 4B Tracker |
| Pass predictions NATO 4B | Pass predictions NATO 4B |
| Orbit launches |
1993-12-08 (32 years ago)
|
| Days in orbit | 11961 |
| Country/organisation of origin | North Atlantic Treaty Organization (NATO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36263 km |
| Apogee | 36307 km |
| Orbit slope (inclination) | 12.97° |
| Laps per day | 1 |
| Height NATO 4B | 36285.56 km |
Additional information NATO 4B
NATO 4B, 22921 is a payload satellite owned by NATO (NATO) in GEO that was launched on Wed, 08 Dec 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 NATO 4B Date of exalting 08.12.1993y. Average height of ISS NATO 4B hundred 36285.56 km. Average velocity NATO 4B is 11004.05 km/h. Inclination NATO 4B satellite 12.96°.TLE
Average velocity NATO 4B
Average inclination NATO 4B
Mean right ascension of the ascending node (RAAN) NATO 4B
Mean argument of perigee NATO 4B
Mean semi-major axis of the orbit NATO 4B
Mean orbital eccentricity NATO 4B
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