TDRS-L in its payload shroud, being hoisted atop its Atlas V launcher
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Mission type | Communications |
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Operator | NASA |
COSPAR ID | 2014-004A |
SATCAT no. | 39504 |
Mission duration | 15 years (planned) |
Spacecraft properties | |
Bus | BSS-601HP |
Manufacturer | Boeing |
Launch mass | 3,454 kg (7,615 lb) |
Start of mission | |
Launch date | January 24, 2014, 02:33:00 | UTC
Rocket | Atlas V 401 |
Launch site | Cape Canaveral SLC-41 |
Contractor | United Launch Alliance |
Orbital parameters | |
Reference system | Geocentric |
Regime | Geosynchronous orbit |
Perigee | 35,785 kilometers (22,236 mi) |
Apogee | 35,797 kilometers (22,243 mi) |
Inclination | 6.77 degrees |
Period | 1436.03 minutes |
Epoch | January 22, 2015, 07:10:47 UTC |
TDRS-12, known before launch as TDRS-L, is an American communications satellite operated by NASA as part of the Tracking and Data Relay Satellite System. The twelfth Tracking and Data Relay Satellite, it is the second third-generation spacecraft to be launched, following TDRS-11 in 2013.
TDRS-12 was constructed by Boeing, based on the BSS-601HP satellite bus. Fully fueled, it has a mass of 3,454 kg (7,615 lb), with a design life of 15 years. It carries two steerable antennae capable of providing S, Ku and Ka band communications for other spacecraft, with an additional array of S-band transponders for lower-rate communications with five further satellites. The satellite is powered by two solar arrays, which produce 2.8 to 3.2 kilowatts of power, while an R-4D-11-300 engine is present to provide propulsion.
The United Launch Alliance was contracted to launch TDRS-12. The spacecraft was launched on January 24, 2014 at 02:33 UTC (21:33 local time on January 23). An Atlas V rocket was used, flying in the 401 configuration, with tail number AV-042.After launch, TDRS-12 was deployed into a high-perigee geosynchronous transfer orbit. The spacecraft raised itself into a geosynchronous orbit using its onboard propulsion system.