OV2-3
Satellite information OV2-3
| Spacetrack Directory Name | OV2-3 |
| Follow OV2-3 | OV2-3 Tracker |
| Pass predictions OV2-3 | Pass predictions OV2-3 |
| Orbit launches |
1965-12-21 (60 years ago)
|
| Days in orbit | 22178 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 251 km |
| Apogee | 16990 km |
| Orbit slope (inclination) | 26.63° |
| Laps per day | 5 |
| Height OV2-3 | 9320 km |
Additional information OV2-3
OV2-3, 13912 is a payload satellite owned by USAF SSD (US) in HEO that was launched on Tue, 21 Dec 1965 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 OV2-3 Date of exalting 21.12.1965y. Average height of ISS OV2-3 hundred 9320 km. Average velocity OV2-3 is 17940.51 km/h. Inclination OV2-3 satellite 26.65°.TLE
Average velocity OV2-3
Average inclination OV2-3
Mean right ascension of the ascending node (RAAN) OV2-3
Mean argument of perigee OV2-3
Mean semi-major axis of the orbit OV2-3
Mean orbital eccentricity OV2-3
ISS
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