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(Redirected from Tianlian II)Tracking and Data Relay Satellite System
Tianlian (Simplified Chinese: 天链, Traditional Chinese: 天鏈, English: Sky Link) also known as CTDRS, is a Chinese data relay communication satellite constellation. The constellation serves to relay data from ground stations to spacecraft and rockets, most significantly China's crewed spaceflight program. The system currently consists of ten satellites in two generations, with the first satellite being launched in 2008.
Tianlian is used to provide real-time communications between orbiting satellites and ground control stations. The Chinese tracking and data relay satellites were developed by the China Academy of Space Technology (CAST) and it is similar to the American Tracking and Data Relay Satellite System (TDRSS) in concept. The system is designed to support near-real-time communications between orbiting spacecraft and ground control, as well as complement the ground-based space tracking and telemetry stations and ships in tracking spacecraft.[1] This is necessary because ground stations can only maintain contact with a satellite while it is overhead. Positioning multiple satellites in geostationary orbit ensures that the ground station and satellite are both always in view of at least one relay satellite, allowing for constant communication between the ground station and target satellite. The system provides data relay services for crewed Shenzhou missions, from Shenzhou 7 onwards, the Tiangong space station, and interplanetary missions.[2][3][4] All satellites were launched from the Xichang Satellite Launch Center and operate in geostationary orbit.[5][6][7][8]
Tianlian I consists of five satellites, all based on the DFH-3 satellite bus. The first satellite of the series, Tianlian I-01, was launched on the maiden flight of the Long March 3C launch vehicle on 25 April 2008.[9][10] With the launch of Tianlian I-03, a spacecraft could be tracked for 70% of its orbit, compared to only 15% without the constellation.[11]
Tianlian II is the second generation of the constellation and currently consists of 5 satellites based on the DFH-4 satellite bus. The second generation system greatly improves data transmission rates and its multi-targeting ability. This in turn improves spacecraft operational safety and flexibility.[12][13]
Satellite Simplified Chinese Name Launch (UTC)[14] Carrier Rocket[14] Launch Site[14] Bus Longitude[15] Status COSPAR ID SATCAT no. First Generation Tianlian I-01 天链一号01星 25 April 2008, 15:35 Long March 3C XSLC LC-2 DFH-3 77.0° East Inactive 2008-019A 32779 Tianlian I-02 天链一号02星 11 July 2011, 15:41 Long March 3C XSLC LC-2 DFH-3 176.72° East Inactive 2011-032A 37737 Tianlian I-03 天链一号03星 25 July 2012, 15:43 Long March 3C XSLC LC-2 DFH-3 16.86° East Inactive 2012-040A 38730 Tianlian I-04 天链一号04星 22 November 2016, 15:24 Long March 3C XSLC LC-2 DFH-3 76.95° East Active 2016-072A 41869 Tianlian I-05 天链一号05星 6 July 2021, 15:53 Long March 3C XSLC LC-2 DFH-3 106.2653° East Active 2021-063A 49011 Second Generation Tianlian II-01 天链二号01星 31 March 2019, 15:51 Long March 3B XSLC LC-2 DFH-4 79.9° East Active 2019-017A 44076 Tianlian II-02 天链二号02星 13 December 2021, 16:09 Long March 3B XSLC LC-3 DFH-4 171.04° East Active 2021-124A 50005 Tianlian II-03 天链二号03星 12 July 2022, 16:30 Long March 3B XSLC LC-2 DFH-4 10.5° East Active 2022-078A 53100 Tianlian II-04 天链二号04星 26 March 2025, 15:55 Long March 3B XSLC LC-2 DFH-4 80.0° East Active 2025-062A 63361 Tianlian II-05 天链二号05星 27 April 2025, 15:54 Long March 3B XSLC LC-2 DFH-4 ActiveWikinews has related news:
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
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