OPS 9345 (IDSCS 23)
Satellite information OPS 9345 (IDSCS 23) - OPS 9345 (IDSCS 24)
| Spacetrack Directory Name | OPS 9345 (IDSCS 23) |
| Alternative name | OPS 9345 (IDSCS 24) |
| Follow OPS 9345 (IDSCS 23) | OPS 9345 (IDSCS 23) Tracker |
| Pass predictions OPS 9345 (IDSCS 23) | Pass predictions OPS 9345 (IDSCS 23) |
| Orbit launches |
1968-06-13 (58 years ago)
|
| Days in orbit | 21273 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 33747 km |
| Apogee | 34014 km |
| Orbit slope (inclination) | 7.26° |
| Laps per day | 1 |
| Height OPS 9345 (IDSCS 23) | 33879.2 km |
Additional information OPS 9345 (IDSCS 23)
OPS 9345 (IDSCS 23), 3288 is a payload satellite owned by SAMSO (US) in GEO that was launched on Thu, 13 Jun 1968 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 9345 (IDSCS 23) Date of exalting 13.06.1968y. Average height of ISS OPS 9345 (IDSCS 23) hundred 33879.2 km. Average velocity OPS 9345 (IDSCS 23) is 11328.24 km/h. Inclination OPS 9345 (IDSCS 23) satellite 7.24°.TLE
Average velocity OPS 9345 (IDSCS 23)
Average inclination OPS 9345 (IDSCS 23)
Mean right ascension of the ascending node (RAAN) OPS 9345 (IDSCS 23)
Mean argument of perigee OPS 9345 (IDSCS 23)
Mean semi-major axis of the orbit OPS 9345 (IDSCS 23)
Mean orbital eccentricity OPS 9345 (IDSCS 23)
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