CHUANGXIN 16B (CX-16B) - Norad Identifikationsnummer: 53876
Name im Katalog Spacetrack | CHUANG XIN 16B (CX-16B) |
Alternative Bezeichnung | CHUANGXIN 16B (CX-16B) |
Folge CHUANG XIN 16B (CX-16B) | CHUANG XIN 16B (CX-16B) Tracker |
Flugzeiten CHUANG XIN 16B (CX-16B) | Flugzeiten CHUANG XIN 16B (CX-16B) |
In die Umlaufbahn bringen |
![]() |
Tage im Orbit | 1006 |
Herkunftsland/-organisation | Chiny (PRC) |
Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | XICLF (Xichang Launch Facility, China) |
Perygeum | 589 km |
Apogäum | 596 km |
Neigung der Umlaufbahn (Inklination) | 28.99° |
Runden pro Tag | 15 |
Höhe CHUANG XIN 16B (CX-16B) | 538.24 km |
CHUANG XIN 16B (CX-16B), 53876 is a payload satellite owned by IMI/CAS (CN) in LEO that was launched on Tue, 23 Aug 2022 UTC via a KUAIZHOU-1A launch vehicle from the Xichang Space Center, China (XSC). 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 CHUANG XIN 16B (CX-16B) hinausgetragen 23.08.2022r. Durchschnittshöhe CHUANG XIN 16B (CX-16B) Text Nummer 1: das. 538.24 km. Durchschnittsgeschwindigkeit CHUANG XIN 16B (CX-16B) beträgt 27346.76 km/h. Neigung CHUANG XIN 16B (CX-16B) Satelliten 28.99°.