OPS 9326 (IDSCS 13)
Satellite information OPS 9326 (IDSCS 13)
| Spacetrack Directory Name | OPS 9326 (IDSCS 13) |
| Follow OPS 9326 (IDSCS 13) | OPS 9326 (IDSCS 13) Tracker |
| Pass predictions OPS 9326 (IDSCS 13) | Pass predictions OPS 9326 (IDSCS 13) |
| Orbit launches |
1967-01-18 (59 years ago)
|
| Days in orbit | 21785 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| WWW | Here |
| Perigee | 33622 km |
| Apogee | 34003 km |
| Orbit slope (inclination) | 8.34° |
| Laps per day | 1 |
| Height OPS 9326 (IDSCS 13) | 33811.48 km |
Additional information OPS 9326 (IDSCS 13)
OPS 9326 (IDSCS 13), 2653 is a payload satellite owned by USAF SSD (US) in GEO that was launched on Wed, 18 Jan 1967 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 9326 (IDSCS 13) Date of exalting 18.01.1967y. Average height of ISS OPS 9326 (IDSCS 13) hundred 33811.48 km. Average velocity OPS 9326 (IDSCS 13) is 11337.86 km/h. Inclination OPS 9326 (IDSCS 13) satellite 8.3°.TLE
Average velocity OPS 9326 (IDSCS 13)
Average inclination OPS 9326 (IDSCS 13)
Mean right ascension of the ascending node (RAAN) OPS 9326 (IDSCS 13)
Mean argument of perigee OPS 9326 (IDSCS 13)
Mean semi-major axis of the orbit OPS 9326 (IDSCS 13)
Mean orbital eccentricity OPS 9326 (IDSCS 13)
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