OPS 9346 (IDSCS 24)
Satellite information OPS 9346 (IDSCS 24) - OPS 9346 (IDSCS 25)
| Spacetrack Directory Name | OPS 9346 (IDSCS 24) |
| Alternative name | OPS 9346 (IDSCS 25) |
| Follow OPS 9346 (IDSCS 24) | OPS 9346 (IDSCS 24) Tracker |
| Pass predictions OPS 9346 (IDSCS 24) | Pass predictions OPS 9346 (IDSCS 24) |
| Orbit launches |
1968-06-13 (58 years ago)
|
| Days in orbit | 21317 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 33750 km |
| Apogee | 34106 km |
| Orbit slope (inclination) | 7.34° |
| Laps per day | 1 |
| Height OPS 9346 (IDSCS 24) | 33928.46 km |
Additional information OPS 9346 (IDSCS 24)
OPS 9346 (IDSCS 24), 3289 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 9346 (IDSCS 24) Date of exalting 13.06.1968y. Average height of ISS OPS 9346 (IDSCS 24) hundred 33928.46 km. Average velocity OPS 9346 (IDSCS 24) is 11321.13 km/h. Inclination OPS 9346 (IDSCS 24) satellite 7.23°.TLE
Average velocity OPS 9346 (IDSCS 24)
Average inclination OPS 9346 (IDSCS 24)
Mean right ascension of the ascending node (RAAN) OPS 9346 (IDSCS 24)
Mean argument of perigee OPS 9346 (IDSCS 24)
Mean semi-major axis of the orbit OPS 9346 (IDSCS 24)
Mean orbital eccentricity OPS 9346 (IDSCS 24)
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