Tianlian (original) (raw)

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Tracking and Data Relay Satellite System

Tianlian

Manufacturer China Academy of Space Technology (CAST)
Country of origin China
Operator China Aerospace Science and Technology Corporation (CASC)
Applications Tracking and Data Relay Satellite System
Specifications
Bus DFH-3 - first generation DFH-4 - second generation
Regime Geostationary
Production
Status In service
Launched 8
Operational 8
Maiden launch Tianlian I-0125 April 2008
Last launch Tianlian II-0312 July 2022

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 seven 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 3 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 Active 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 Active 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 Active 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-3 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 Active 2022-078A 53100