OAO 2
Satellite information OAO 2
| Spacetrack Directory Name | OAO 2 |
| Follow OAO 2 | OAO 2 Tracker |
| Pass predictions OAO 2 | Pass predictions OAO 2 |
| Orbit launches |
1968-12-07 (57 years ago)
|
| Days in orbit | 21096 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 736 km |
| Apogee | 743 km |
| Orbit slope (inclination) | 34.99° |
| Laps per day | 14 |
| Height OAO 2 | 736.2 km |
Additional information OAO 2
OAO 2, 3597 is a payload satellite owned by GSFC (US) in LEO that was launched on Sat, 07 Dec 1968 UTC via an ATLAS SLV-3C CENTAUR 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 OAO 2 Date of exalting 07.12.1968y. Average height of ISS OAO 2 hundred 736.2 km. Average velocity OAO 2 is 26962.19 km/h. Inclination OAO 2 satellite 34.99°.TLE
Average velocity OAO 2
Average inclination OAO 2
Mean right ascension of the ascending node (RAAN) OAO 2
Mean argument of perigee OAO 2
Mean semi-major axis of the orbit OAO 2
Mean orbital eccentricity OAO 2
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