CALSPHERE 4(A)
Informationen über den Satelliten. CALSPHERE 4(A)
| Name im Katalog Spacetrack | CALSPHERE 4(A) |
| Folge CALSPHERE 4(A) | CALSPHERE 4(A) Tracker |
| Flugzeiten CALSPHERE 4(A) | Flugzeiten CALSPHERE 4(A) |
| In die Umlaufbahn bringen |
1965-08-13 (60 vor Jahren)
|
| Tage im Orbit | 22093 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFWTR (Vandenberg Air Force Base, USA) |
| Perygeum | 1074 km |
| Apogäum | 1176 km |
| Neigung der Umlaufbahn (Inklination) | 89.91° |
| Runden pro Tag | 13 |
| Höhe CALSPHERE 4(A) | 1135.71 km |
Informationen über CALSPHERE 4(A)
CALSPHERE 4(A), 1520 is a payload satellite owned by NRL (US) in LEO that was launched on Fri, 13 Aug 1965 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 4(A) hinausgetragen 13.08.1965r. Durchschnittshöhe CALSPHERE 4(A) Text Nummer 1: das. 1135.71 km. Durchschnittsgeschwindigkeit CALSPHERE 4(A) beträgt 26231.78 km/h. Neigung CALSPHERE 4(A) Satelliten 89.93°.Orbital Elemente
Durchschnittshöhe der Orbitalbahn. CALSPHERE 4(A)
Durchschnittsgeschwindigkeit CALSPHERE 4(A)
Durchschnitt CALSPHERE 4(A)
