2022-102A - Norad Identifikationsnummer: 53586
| Name im Katalog Spacetrack | CHUANG XIN 16A (CX-16A) |
| Alternative Bezeichnung | 2022-102A |
| Folge CHUANG XIN 16A (CX-16A) | CHUANG XIN 16A (CX-16A) Tracker |
| Flugzeiten CHUANG XIN 16A (CX-16A) | Flugzeiten CHUANG XIN 16A (CX-16A) |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 1211 |
| Herkunftsland/-organisation | Chiny (PRC) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | XICLF (Xichang Launch Facility, China) |
| Perygeum | 590 km |
| Apogäum | 596 km |
| Neigung der Umlaufbahn (Inklination) | 29° |
| Runden pro Tag | 15 |
| Höhe CHUANG XIN 16A (CX-16A) | 557.38 km |
CHUANG XIN 16A (CX-16A), 53586 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 16A (CX-16A) hinausgetragen 23.08.2022r. Durchschnittshöhe CHUANG XIN 16A (CX-16A) Text Nummer 1: das. 557.38 km. Durchschnittsgeschwindigkeit CHUANG XIN 16A (CX-16A) beträgt 27308.89 km/h. Neigung CHUANG XIN 16A (CX-16A) Satelliten 29°.