OPS 9346 (IDSCS 25) - Norad Identifikationsnummer: 3289
| Name im Katalog Spacetrack | OPS 9346 (IDSCS 24) |
| Alternative Bezeichnung | OPS 9346 (IDSCS 25) |
| Folge OPS 9346 (IDSCS 24) | OPS 9346 (IDSCS 24) Tracker |
| Flugzeiten OPS 9346 (IDSCS 24) | Flugzeiten OPS 9346 (IDSCS 24) |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 21332 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perygeum | 33750 km |
| Apogäum | 34106 km |
| Neigung der Umlaufbahn (Inklination) | 7.37° |
| Runden pro Tag | 1 |
| Höhe OPS 9346 (IDSCS 24) | 33928.4 km |
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.
der Satellit OPS 9346 (IDSCS 24) hinausgetragen 13.06.1968r. Durchschnittshöhe OPS 9346 (IDSCS 24) Text Nummer 1: das. 33928.4 km. Durchschnittsgeschwindigkeit OPS 9346 (IDSCS 24) beträgt 11321.15 km/h. Neigung OPS 9346 (IDSCS 24) Satelliten 7.25°.