OPS 1527 (OV3-1)
Satellite information OPS 1527 (OV3-1)
| Spacetrack Directory Name | OPS 1527 (OV3-1) |
| Follow OPS 1527 (OV3-1) | OPS 1527 (OV3-1) Tracker |
| Pass predictions OPS 1527 (OV3-1) | Pass predictions OPS 1527 (OV3-1) |
| Orbit launches |
1966-04-22 (60 years ago)
|
| Days in orbit | 22049 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 334 km |
| Apogee | 2932 km |
| Orbit slope (inclination) | 82.37° |
| Laps per day | 13 |
| Height OPS 1527 (OV3-1) | 1491.29 km |
Additional information OPS 1527 (OV3-1)
OPS 1527 (OV3-1), 2150 is a payload satellite owned by USAF OAR (US) in LEO that was launched on Fri, 22 Apr 1966 UTC via an SCOUT B 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 OPS 1527 (OV3-1) Date of exalting 22.04.1966y. Average height of ISS OPS 1527 (OV3-1) hundred 1491.29 km. Average velocity OPS 1527 (OV3-1) is 25631.95 km/h. Inclination OPS 1527 (OV3-1) satellite 82.37°.TLE
Average velocity OPS 1527 (OV3-1)
Average inclination OPS 1527 (OV3-1)
Mean right ascension of the ascending node (RAAN) OPS 1527 (OV3-1)
Mean argument of perigee OPS 1527 (OV3-1)
Mean semi-major axis of the orbit OPS 1527 (OV3-1)
Mean orbital eccentricity OPS 1527 (OV3-1)
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