OV2-5
Satellite information OV2-5
| Spacetrack Directory Name | OV2-5 |
| Follow OV2-5 | OV2-5 Tracker |
| Pass predictions OV2-5 | Pass predictions OV2-5 |
| Orbit launches |
1968-09-26 (57 years ago)
|
| Days in orbit | 21168 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35066 km |
| Apogee | 35792 km |
| Orbit slope (inclination) | 2.18° |
| Laps per day | 1 |
| Height OV2-5 | 35430.97 km |
Additional information OV2-5
OV2-5, 3428 is a payload satellite owned by SAMSO (US) in GEO that was launched on Thu, 26 Sep 1968 UTC via a TITAN IIIC 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 OV2-5 Date of exalting 26.09.1968y. Average height of ISS OV2-5 hundred 35430.97 km. Average velocity OV2-5 is 11115.83 km/h. Inclination OV2-5 satellite 2.15°.TLE
Average velocity OV2-5
Average inclination OV2-5
Mean right ascension of the ascending node (RAAN) OV2-5
Mean argument of perigee OV2-5
Mean semi-major axis of the orbit OV2-5
Mean orbital eccentricity OV2-5
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