OPS 9312 (IDSCS 2)
Satellite information OPS 9312 (IDSCS 2)
| Spacetrack Directory Name | OPS 9312 (IDSCS 2) |
| Follow OPS 9312 (IDSCS 2) | OPS 9312 (IDSCS 2) Tracker |
| Pass predictions OPS 9312 (IDSCS 2) | Pass predictions OPS 9312 (IDSCS 2) |
| Orbit launches |
1966-06-16 (60 years ago)
|
| Days in orbit | 22001 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 33670 km |
| Apogee | 33904 km |
| Orbit slope (inclination) | 8.81° |
| Laps per day | 1 |
| Height OPS 9312 (IDSCS 2) | 33786.82 km |
Additional information OPS 9312 (IDSCS 2)
OPS 9312 (IDSCS 2), 2216 is a payload satellite owned by USAF SSD (US) in GEO that was launched on Thu, 16 Jun 1966 UTC via a TITAN IIIC launch vehicle from the Air Force Eastern Test Range (AFETR). 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 9312 (IDSCS 2) Date of exalting 16.06.1966y. Average height of ISS OPS 9312 (IDSCS 2) hundred 33786.82 km. Average velocity OPS 9312 (IDSCS 2) is 11341.24 km/h. Inclination OPS 9312 (IDSCS 2) satellite 8.78°.TLE
Average velocity OPS 9312 (IDSCS 2)
Average inclination OPS 9312 (IDSCS 2)
Mean right ascension of the ascending node (RAAN) OPS 9312 (IDSCS 2)
Mean argument of perigee OPS 9312 (IDSCS 2)
Mean semi-major axis of the orbit OPS 9312 (IDSCS 2)
Mean orbital eccentricity OPS 9312 (IDSCS 2)
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