OV1-2
Satellite information OV1-2
| Spacetrack Directory Name | OV1-2 |
| Follow OV1-2 | OV1-2 Tracker |
| Pass predictions OV1-2 | Pass predictions OV1-2 |
| Orbit launches |
1965-10-05 (60 years ago)
|
| Days in orbit | 22248 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 399 km |
| Apogee | 2290 km |
| Orbit slope (inclination) | 144.23° |
| Laps per day | 13 |
| Height OV1-2 | 1305.04 km |
Additional information OV1-2
OV1-2, 1613 is a payload satellite owned by USAF OAR (US) in LEO that was launched on Tue, 05 Oct 1965 UTC via an ATLAS D launch vehicle from the Air Force Western Test Range (AFWTR). 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 OV1-2 Date of exalting 05.10.1965y. Average height of ISS OV1-2 hundred 1305.04 km. Average velocity OV1-2 is 25944.43 km/h. Inclination OV1-2 satellite 144.23°.TLE
Average velocity OV1-2
Average inclination OV1-2
Mean right ascension of the ascending node (RAAN) OV1-2
Mean argument of perigee OV1-2
Mean semi-major axis of the orbit OV1-2
Mean orbital eccentricity OV1-2
ISS
Buy us a coffee!
