NATO 3A
Satellite information NATO 3A
| Spacetrack Directory Name | NATO 3A |
| Follow NATO 3A | NATO 3A Tracker |
| Pass predictions NATO 3A | Pass predictions NATO 3A |
| Orbit launches |
1976-04-22 (50 years ago)
|
| Days in orbit | 18402 |
| Country/organisation of origin | North Atlantic Treaty Organization (NATO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35811 km |
| Apogee | 36005 km |
| Orbit slope (inclination) | 4.8° |
| Laps per day | 1 |
| Height NATO 3A | 35904.93 km |
Additional information NATO 3A
NATO 3A, 8808 is a payload satellite owned by NICSMA (NATO) in GEO that was launched on Thu, 22 Apr 1976 UTC via a DELTA 2914 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 3A Date of exalting 22.04.1976y. Average height of ISS NATO 3A hundred 35904.93 km. Average velocity NATO 3A is 11053.4 km/h. Inclination NATO 3A satellite 4.83°.TLE
Average velocity NATO 3A
Average inclination NATO 3A
Mean right ascension of the ascending node (RAAN) NATO 3A
Mean argument of perigee NATO 3A
Mean semi-major axis of the orbit NATO 3A
Mean orbital eccentricity NATO 3A
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