OPS 1427 (OV3-4)
Satellite information OPS 1427 (OV3-4)
| Spacetrack Directory Name | OPS 1427 (OV3-4) |
| Follow OPS 1427 (OV3-4) | OPS 1427 (OV3-4) Tracker |
| Pass predictions OPS 1427 (OV3-4) | Pass predictions OPS 1427 (OV3-4) |
| Orbit launches |
1966-06-10 (60 years ago)
|
| Days in orbit | 22017 |
| Country/organisation of origin | USA (US) |
| Starting point | WLPIS (Wallops Island) |
| Perigee | 641 km |
| Apogee | 4686 km |
| Orbit slope (inclination) | 40.89° |
| Laps per day | 10 |
| Height OPS 1427 (OV3-4) | 2890.46 km |
Additional information OPS 1427 (OV3-4)
OPS 1427 (OV3-4), 2201 is a payload satellite owned by USAF OAR (US) in LEO that was launched on Fri, 10 Jun 1966 UTC via an SCOUT B launch vehicle from the Wallops Island (WLPIS). 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 1427 (OV3-4) Date of exalting 10.06.1966y. Average height of ISS OPS 1427 (OV3-4) hundred 2890.46 km. Average velocity OPS 1427 (OV3-4) is 23608.52 km/h. Inclination OPS 1427 (OV3-4) satellite 40.9°.TLE
Average velocity OPS 1427 (OV3-4)
Average inclination OPS 1427 (OV3-4)
Mean right ascension of the ascending node (RAAN) OPS 1427 (OV3-4)
Mean argument of perigee OPS 1427 (OV3-4)
Mean semi-major axis of the orbit OPS 1427 (OV3-4)
Mean orbital eccentricity OPS 1427 (OV3-4)
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