NATO 2B
Satellite information NATO 2B
| Spacetrack Directory Name | NATO 2B |
| Follow NATO 2B | NATO 2B Tracker |
| Pass predictions NATO 2B | Pass predictions NATO 2B |
| Orbit launches |
1971-02-03 (55 years ago)
|
| Days in orbit | 20307 |
| Country/organisation of origin | North Atlantic Treaty Organization (NATO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35774 km |
| Apogee | 35799 km |
| Orbit slope (inclination) | 0.96° |
| Laps per day | 1 |
| Height NATO 2B | 35786.11 km |
Additional information NATO 2B
NATO 2B, 4902 is a payload satellite owned by NATO (NATO) in GEO that was launched on Wed, 03 Feb 1971 UTC via a THOR DELTA M 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 2B Date of exalting 03.02.1971y. Average height of ISS NATO 2B hundred 35786.11 km. Average velocity NATO 2B is 11068.98 km/h. Inclination NATO 2B satellite 0.99°.TLE
Average velocity NATO 2B
Average inclination NATO 2B
Mean right ascension of the ascending node (RAAN) NATO 2B
Mean argument of perigee NATO 2B
Mean semi-major axis of the orbit NATO 2B
Mean orbital eccentricity NATO 2B
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