CALSPHERE 2
Informationen über den Satelliten. CALSPHERE 2
| Name im Katalog Spacetrack | CALSPHERE 2 |
| Folge CALSPHERE 2 | CALSPHERE 2 Tracker |
| Flugzeiten CALSPHERE 2 | Flugzeiten CALSPHERE 2 |
| In die Umlaufbahn bringen |
1964-10-06 (60 vor Jahren)
|
| Tage im Orbit | 22185 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFWTR (Vandenberg Air Force Base, USA) |
| Perygeum | 1049 km |
| Apogäum | 1075 km |
| Neigung der Umlaufbahn (Inklination) | 90.23° |
| Runden pro Tag | 14 |
| Höhe CALSPHERE 2 | 1074.12 km |
Informationen über CALSPHERE 2
CALSPHERE 2, 902 is a payload satellite owned by NRL (US) in LEO that was launched on Tue, 06 Oct 1964 UTC via a THOR ABLESTAR launch vehicle from the Air Force Western Test Range (AFWTR). 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 CALSPHERE 2 hinausgetragen 06.10.1964r. Durchschnittshöhe CALSPHERE 2 Text Nummer 1: das. 1074.12 km. Durchschnittsgeschwindigkeit CALSPHERE 2 beträgt 26339.64 km/h. Neigung CALSPHERE 2 Satelliten 90.22°.Orbital Elemente
Durchschnittshöhe der Orbitalbahn. CALSPHERE 2
Durchschnittsgeschwindigkeit CALSPHERE 2
Durchschnitt CALSPHERE 2
