YAOGAN 17A
Informationen über den Satelliten. YAOGAN 17A
| Name im Katalog Spacetrack | YAOGAN 17A |
| Folge YAOGAN 17A | YAOGAN 17A Tracker |
| Flugzeiten YAOGAN 17A | Flugzeiten YAOGAN 17A |
| In die Umlaufbahn bringen |
2013-09-01 (11 vor Jahren)
|
| Tage im Orbit | 4298 |
| Herkunftsland/-organisation | Chiny (PRC) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | JSC (Jiuquan Satellite Launch Center, China) |
| Kategorie | |
| Perygeum | 905 km |
| Apogäum | 1275 km |
| Neigung der Umlaufbahn (Inklination) | 63.39° |
| Runden pro Tag | 13 |
| Orbit | LEO (Nicht-polar geneigt) |
| Höhe YAOGAN 17A | 1104.12 km |
Informationen über YAOGAN 17A
Yaogan (Chinese: ????; pinyin: Yáog?n w?ix?ng; literally: 'Remote Sensing Satellite') is a series of Chinese reconnaissance satellites launched in the early 21st century.
Chinese media describe the satellites as intended for "scientific experiments, land survey, crop yield assessment, and disaster monitoring". Western analysts suspect that they are also used for military purposes. Analysts believe that each satellite employs either optical or synthetic aperture radar (SAR) sensors and that the SAR satellites are of the Jian Bing-5 series.The SAR satellite was developed by the Shanghai Academy of Space Flight Technology (SAST). The electro-optical digital imaging satellite was developed by the China Academy of Space Technology (CAST). It is carried into space atop a Chang Zheng (Long March) rocket.Yaogan satellites have been launched from both the Taiyuan Satellite Launch Center in China's northern Shanxi province and the Jiuquan Satellite Launch Center in China's northwestern Gansu province.
Orbital Elemente
Durchschnittshöhe der Orbitalbahn. YAOGAN 17A
Durchschnittsgeschwindigkeit YAOGAN 17A
Durchschnitt YAOGAN 17A
