OPS 1920
Satellite information OPS 1920
| Spacetrack Directory Name | OPS 1920 |
| Follow OPS 1920 | OPS 1920 Tracker |
| Pass predictions OPS 1920 | Pass predictions OPS 1920 |
| Orbit launches |
1966-10-05 (59 years ago)
|
| Days in orbit | 21883 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 3658 km |
| Apogee | 3723 km |
| Orbit slope (inclination) | 89.85° |
| Laps per day | 9 |
| Height OPS 1920 | 3702.7 km |
Additional information OPS 1920
OPS 1920, 2481 is a payload satellite owned by USAF SSD (US) in LEO that was launched on Wed, 05 Oct 1966 UTC via an ATLAS SLV-3 AGENA 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 OPS 1920 Date of exalting 05.10.1966y. Average height of ISS OPS 1920 hundred 3702.7 km. Average velocity OPS 1920 is 22645.56 km/h. Inclination OPS 1920 satellite 89.85°.TLE
Average velocity OPS 1920
Average inclination OPS 1920
Mean right ascension of the ascending node (RAAN) OPS 1920
Mean argument of perigee OPS 1920
Mean semi-major axis of the orbit OPS 1920
Mean orbital eccentricity OPS 1920
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