TIANLIAN 1-01
Informationen über den Satelliten. TIANLIAN 1-01
| Name im Katalog Spacetrack | TIANLIAN 1-01 |
| Folge TIANLIAN 1-01 | TIANLIAN 1-01 Tracker |
| Flugzeiten TIANLIAN 1-01 | Flugzeiten TIANLIAN 1-01 |
| In die Umlaufbahn bringen |
2008-04-25 (18 vor Jahren)
|
| Tage im Orbit | 6768 |
| Herkunftsland/-organisation | Chiny (PRC) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | XICLF (Xichang Launch Facility, China) |
| WWW | hier |
| Kategorie | |
| Perygeum | 35651 km |
| Apogäum | 35922 km |
| Neigung der Umlaufbahn (Inklination) | 10.49° |
| Runden pro Tag | 1 |
| Orbit | GEO |
| Höhe TIANLIAN 1-01 | 36607.1 km |
Informationen über TIANLIAN 1-01
Tianlian I (Simplified Chinese: ????, Traditional Chinese: ????, English: Sky Chain), also known as Tian Lian 1, TL-1, and CTDRS-1 is a Chinese data tracking and relay communications satellite series. Based on the DFH-3 satellite bus, it will provide communication coverage for manned Shenzhou missions, from Shenzhou 7 onwards. Functionally, it is similar to the United States Tracking and Data Relay Satellite System.
The first satellite of the series, Tianlian I-01, was launched on the maiden flight of the Long March 3C carrier rocket, at 15:35 GMT on 25 April 2008, from LC-2 at the Xichang Satellite Launch Centre. Tianlian I-01 is able to cover around half of the spacecraft's trajectory, compared to around 12 percent which had been covered using tracking stations and a fleet of ships. Tianlian I-02 was launched on 11 July 2011, Tianlian I-03 on 25 July 2012 and Tianlian I-04 on 22 November 2016. The satellites are in geostationary orbit.
Orbital Elemente
Durchschnittshöhe der Orbitalbahn. TIANLIAN 1-01
Durchschnittsgeschwindigkeit TIANLIAN 1-01
Durchschnitt TIANLIAN 1-01
Mittlere Rektaszension des aufsteigenden Knotens (RAAN) TIANLIAN 1-01
Mittleres Argument des Perigäums TIANLIAN 1-01
Mittlere große Halbachse der Umlaufbahn TIANLIAN 1-01
Mittlere Bahnexzentrizität TIANLIAN 1-01
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