Mission type | Navigation |
---|---|
Operator | US Air Force |
COSPAR ID | 2015-013A [1] |
SATCAT no. | 40534 [1] |
Mission duration | 12 years (planned) |
Spacecraft properties | |
Spacecraft | GPS SVN-71 (IIF-9) |
Spacecraft type | GPS Block IIF |
Manufacturer | Boeing |
Launch mass | 1,630 kilograms (3,590 lb) [2] |
Start of mission | |
Launch date | 25 March 2015, 18:36 | UTC
Rocket | Delta IV-M+(4,2), D371 [3] |
Launch site | Cape Canaveral SLC-37B [3] |
Contractor | ULA |
Orbital parameters | |
Reference system | Geocentric |
Regime |
Medium Earth ( Semi-synchronous) |
Perigee altitude | 20,445 km (12,704 mi) [4] |
Apogee altitude | 20,468 km (12,718 mi) [4] |
Inclination | 55.00 degrees [4] |
Period | 729.14 minutes [4] |
Epoch | 25 March 2015, 23:57:44 UTC |
USA-260, also known as GPS IIF-9, GPS SVN-71 and NAVSTAR 73, is an American Satellite navigation which forms part of the Global Positioning System. It was the ninth of twelve Block IIF satellites to be launched. [2]
Built by Boeing and launched by United Launch Alliance, USA-260 was launched at 18:36 UTC on 25 March 2015, atop a Delta IV carrier rocket, flight number D370, flying in the Medium+(4,2) configuration. [3] The launch took place from Space Launch Complex 37B at the Cape Canaveral Air Force Station, [5] and placed USA-260 directly into medium Earth orbit. [4]
On 25 March 2015, USA-260 was in an orbit with a perigee of 20,445 kilometers (12,704 mi), an apogee of 20,468 kilometers (12,718 mi), a period of 729.14 minutes, and 55.00 degrees of inclination to the equator. [4] It is used to broadcast the PRN 26 signal, and operates in slot 5 of plane B 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 April 20, 2015. [6]
Mission type | Navigation |
---|---|
Operator | US Air Force |
COSPAR ID | 2015-013A [1] |
SATCAT no. | 40534 [1] |
Mission duration | 12 years (planned) |
Spacecraft properties | |
Spacecraft | GPS SVN-71 (IIF-9) |
Spacecraft type | GPS Block IIF |
Manufacturer | Boeing |
Launch mass | 1,630 kilograms (3,590 lb) [2] |
Start of mission | |
Launch date | 25 March 2015, 18:36 | UTC
Rocket | Delta IV-M+(4,2), D371 [3] |
Launch site | Cape Canaveral SLC-37B [3] |
Contractor | ULA |
Orbital parameters | |
Reference system | Geocentric |
Regime |
Medium Earth ( Semi-synchronous) |
Perigee altitude | 20,445 km (12,704 mi) [4] |
Apogee altitude | 20,468 km (12,718 mi) [4] |
Inclination | 55.00 degrees [4] |
Period | 729.14 minutes [4] |
Epoch | 25 March 2015, 23:57:44 UTC |
USA-260, also known as GPS IIF-9, GPS SVN-71 and NAVSTAR 73, is an American Satellite navigation which forms part of the Global Positioning System. It was the ninth of twelve Block IIF satellites to be launched. [2]
Built by Boeing and launched by United Launch Alliance, USA-260 was launched at 18:36 UTC on 25 March 2015, atop a Delta IV carrier rocket, flight number D370, flying in the Medium+(4,2) configuration. [3] The launch took place from Space Launch Complex 37B at the Cape Canaveral Air Force Station, [5] and placed USA-260 directly into medium Earth orbit. [4]
On 25 March 2015, USA-260 was in an orbit with a perigee of 20,445 kilometers (12,704 mi), an apogee of 20,468 kilometers (12,718 mi), a period of 729.14 minutes, and 55.00 degrees of inclination to the equator. [4] It is used to broadcast the PRN 26 signal, and operates in slot 5 of plane B 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 April 20, 2015. [6]