OPS 5712 (P/L 152)
Satellite information OPS 5712 (P/L 152)
| Spacetrack Directory Name | OPS 5712 (P/L 152) |
| Follow OPS 5712 (P/L 152) | OPS 5712 (P/L 152) Tracker |
| Pass predictions OPS 5712 (P/L 152) | Pass predictions OPS 5712 (P/L 152) |
| Orbit launches |
1967-05-31 (59 years ago)
|
| Days in orbit | 21645 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 893 km |
| Apogee | 909 km |
| Orbit slope (inclination) | 69.97° |
| Laps per day | 14 |
| Height OPS 5712 (P/L 152) | 909.33 km |
Additional information OPS 5712 (P/L 152)
OPS 5712 (P/L 152), 2873 is an American payload satellite in LEO that was launched on Wed, 31 May 1967 UTC via a THOR SLV-2 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 5712 (P/L 152) Date of exalting 31.05.1967y. Average height of ISS OPS 5712 (P/L 152) hundred 909.33 km. Average velocity OPS 5712 (P/L 152) is 26636.48 km/h. Inclination OPS 5712 (P/L 152) satellite 69.97°.TLE
Average velocity OPS 5712 (P/L 152)
Average inclination OPS 5712 (P/L 152)
Mean right ascension of the ascending node (RAAN) OPS 5712 (P/L 152)
Mean argument of perigee OPS 5712 (P/L 152)
Mean semi-major axis of the orbit OPS 5712 (P/L 152)
Mean orbital eccentricity OPS 5712 (P/L 152)
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