USA-206,[1] also GPS SVN-50, PRN-05 and NAVSTAR 64 and known before launch as GPS IIR-21, GPS IIRM-8 or GPS IIR-21(M), is an American navigation satellite which forms part of the Navstar Global Positioning System. It was the twenty-first and last Block IIR GPS satellite to be launched, and the eighth to use the modernized IIRM configuration.[2]
![]() Artist's impression of a GPS IIRM satellite in orbit | |
Mission type | Navigation |
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Operator | US Air Force |
COSPAR ID | 2009-043A ![]() |
SATCAT no. | 35752 |
Mission duration | 10 years (planned) |
Spacecraft properties | |
Spacecraft type | GPS Block IIRM |
Bus | AS-4000 |
Manufacturer | Lockheed Martin |
Launch mass | 2,032 kilograms (4,480 lb) |
Start of mission | |
Launch date | 17 August 2009, 10:35:00 (2009-08-17UTC10:35Z) UTC |
Rocket | Delta II 7925-9.5, D343 |
Launch site | Cape Canaveral SLC-17A |
Contractor | ULA |
Orbital parameters | |
Reference system | Geocentric |
Regime | Medium Earth (Semi-synchronous) |
Perigee altitude | 20,200 kilometers (12,600 mi) |
Apogee altitude | 20,200 kilometers (12,600 mi) |
Inclination | 55 degrees |
Period | 12 hours |
GPS IIR-21 was built by Lockheed Martin, based on the AS-4000 satellite bus, with the navigation payload being built by ITT.[2] It was launched by a United Launch Alliance Delta II rocket, using the 7925-9.5 configuration,[3] on 17 August 2009 at 10:35 GMT.[4] It was the last spacecraft to launch from Space Launch Complex 17A at the Cape Canaveral Air Force Station, a launch pad which was first used in August 1957 for test flights of the PGM-17 Thor missile.[5] It is also the final flight of an AS-4000 bus,[6] the final GPS launch on a Delta II, and the final Delta II launch to be overseen by the US Air Force.[3]
Following separation from its carrier rocket, GPS IIR-21 received its USA designation, USA-206. It was deployed into a transfer orbit, from which raised itself to a semi-synchronous medium Earth orbit on 19 August, using an onboard Star 37FM apogee motor. It is a 2,032-kilogram (4,480 lb) satellite,[1] and is expected to operate for at least ten years.[3] Once it had completed on-orbit testing, it began covering Slot 3 of Plane E of the GPS constellation, replacing USA-126, or GPS IIA-26, which was launched in July 1996.[4] It was declared operational on 27 August 2009.[7]
NAVSTAR Global Positioning System satellites | |
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List of GPS satellites | |
Block I | |
Block II | |
Block IIA | |
Block IIR | |
Block IIRM | |
Block IIF | |
Block III | |
Block IIIF |
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Italics indicate future missions. Signs † indicate launch failures. |
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Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ). Cubesats are smaller. Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses). |