A Block IIF GPS satellite
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| Mission type | Navigation |
|---|---|
| Operator | US Air Force |
| COSPAR ID | 2015-033A[1] |
| SATCAT no. | 40730[1] |
| Mission duration | 12 years (planned) |
| Spacecraft properties | |
| Spacecraft | GPS SVN-72 (IIF-10) |
| Spacecraft type | GPS Block IIF |
| Manufacturer | Boeing |
| Launch mass | 1,630 kilograms (3,590 lb)[2] |
| Start of mission | |
| Launch date | 15 July 2015, 15:36 (2015-07-15UTC15:36Z) UTC |
| Rocket | Atlas V 401, AV-055[3] |
| Launch site | Cape Canaveral SLC-41[3] |
| Contractor | ULA |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Medium Earth (Semi-synchronous) |
| Perigee altitude | 20,445 km (12,704 mi)[4] |
| Apogee altitude | 20,450 km (12,710 mi)[4] |
| Inclination | 55.00 degrees[4] |
| Period | 728.77 minutes[4] |
| Epoch | 15 July 2015, 21:23:20 UTC |
USA-262, also known as GPS IIF-10, GPS SVN-72 and NAVSTAR 74, is an American navigation satellite which forms part of the Global Positioning System. It was the tenth of twelve Block IIF satellites to be launched.[2]
Built by Boeing and launched by United Launch Alliance, USA-262 was launched at 15:36 UTC on 15 July 2015, atop an Atlas V 401 carrier rocket, vehicle number AV-055.[3] The launch took place from Space Launch Complex 41 at the Cape Canaveral Air Force Station,[5] and placed USA-262 directly into semi-synchronous orbit.[4]
As of 15 July 2015, USA-262 was in an orbit with a perigee of 20,445 kilometers (12,704 mi), an apogee of 20,450 kilometers (12,710 mi), a period of 728.77 minutes, and 55.00 degrees of inclination to the equator.[4] It is used to broadcast the PRN 08 signal, and operates in slot 3 of plane C of the GPS constellation. The satellite has a design life of 15 years and a mass of 1,630 kilograms (3,590 lb). [2] It is currently in service following commissioning on August 12, 2015.[6]
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NAVSTAR Global Positioning System satellites
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| Block I |
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| Block II |
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| Block IIA |
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| Block IIR |
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| Block IIRM |
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| Block IIF |
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| Block III |
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| 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 ( / ). | |
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