NATO 2A
Satellite information NATO 2A
| Spacetrack Directory Name | NATO 2A |
| Follow NATO 2A | NATO 2A Tracker |
| Pass predictions NATO 2A | Pass predictions NATO 2A |
| Orbit launches |
1970-03-20 (56 years ago)
|
| Days in orbit | 20627 |
| Country/organisation of origin | North Atlantic Treaty Organization (NATO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35784 km |
| Apogee | 35787 km |
| Orbit slope (inclination) | 0.32° |
| Laps per day | 1 |
| Height NATO 2A | 35783.86 km |
Additional information NATO 2A
NATO 2A, 4353 is a payload satellite owned by NATO (NATO) in GEO that was launched on Fri, 20 Mar 1970 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 2A Date of exalting 20.03.1970y. Average height of ISS NATO 2A hundred 35783.86 km. Average velocity NATO 2A is 11069.28 km/h. Inclination NATO 2A satellite 0.34°.TLE
Average velocity NATO 2A
Average inclination NATO 2A
Mean right ascension of the ascending node (RAAN) NATO 2A
Mean argument of perigee NATO 2A
Mean semi-major axis of the orbit NATO 2A
Mean orbital eccentricity NATO 2A
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