OPS 9316 (IDSCS 6)
Satellite information OPS 9316 (IDSCS 6)
| Spacetrack Directory Name | OPS 9316 (IDSCS 6) |
| Follow OPS 9316 (IDSCS 6) | OPS 9316 (IDSCS 6) Tracker |
| Pass predictions OPS 9316 (IDSCS 6) | Pass predictions OPS 9316 (IDSCS 6) |
| 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 | 33721 km |
| Apogee | 34200 km |
| Orbit slope (inclination) | 8.61° |
| Laps per day | 1 |
| Height OPS 9316 (IDSCS 6) | 33961.65 km |
Additional information OPS 9316 (IDSCS 6)
OPS 9316 (IDSCS 6), 2220 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 9316 (IDSCS 6) Date of exalting 16.06.1966y. Average height of ISS OPS 9316 (IDSCS 6) hundred 33961.65 km. Average velocity OPS 9316 (IDSCS 6) is 11316.5 km/h. Inclination OPS 9316 (IDSCS 6) satellite 8.6°.TLE
Average velocity OPS 9316 (IDSCS 6)
Average inclination OPS 9316 (IDSCS 6)
Mean right ascension of the ascending node (RAAN) OPS 9316 (IDSCS 6)
Mean argument of perigee OPS 9316 (IDSCS 6)
Mean semi-major axis of the orbit OPS 9316 (IDSCS 6)
Mean orbital eccentricity OPS 9316 (IDSCS 6)
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