The first seven TDRSS satellites were built by the The first tracking and data relay satellite was launched in 1983 on the The second tracking and data relay satellite was destroyed along with "Working solo, TDRS-1 provided more communication coverage, in support of the September 1983 Shuttle mission, than the entire network of NASA tracking stations had provided in all previous Shuttle missions. Spacecraft in the TDRSS require only one communications system, since ground-based telemetry stations will be compatible with TDRSS equipment. Space Network Ground Segment Sustainment (SGSS) Mission System Requirements Document (MSRD). Section 3.5. NASA/GSFC: November 21, 2008 A tracking and data relay satellite is a type of communications satellite that forms part of the Tracking and Data Relay Satellite System used by NASA and other United States government agencies for communications to and from independent "User Platforms" such as satellites, balloons, aircraft, the International Space Station, and remote bases like the Amundsen-Scott South Pole Station. "The first generation of TDRS are planned to be retired in 2015.The communications systems of the TDRSS satellites were designed to support multiple missions at the same time. TDRS-A was the first of TDRSS multiple satellite tracking system. Thus, satellites that are lost in launch failures or have massive malfunctions are never numbered. This system was designed to replace an existing worldwide network of ground stations that had supported all of Each satellite has Note: while a TDRSS satellite is in the manufacturing process it is given a letter designation, but once it has successfully achieved the correct geosynchronous orbit it is referred to with a number (for example, TDRS-A during development and before on-orbit acceptance, and TDRS-1 after acceptance on orbit and put into operational use). The system is a concept utilizing communication satellite technology that improves and economizes the satellite tracking and TDRSS was originally intended to support satellites with apogees below 12,000 km.
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