Nimiq 5
Mission type | Communications |
---|---|
Operator | Telesat Canada |
COSPAR ID | 2009-050A |
SATCAT № | 35873 |
Mission duration | 15 years |
Spacecraft properties | |
Bus | LS-1300 |
Manufacturer | Space Systems/Loral |
Launch mass | 4,745 kilograms (10,461 lb) |
Start of mission | |
Launch date | 17 September 2009, 19:19:19[1] | UTC
Rocket | Proton-M/Briz-M |
Launch site | Baikonur 200/39 |
Contractor | ILS |
Orbital parameters | |
Reference system | Geocentric |
Regime | Geostationary |
Longitude | 72.7° West |
Slot | 73° West |
Perigee | 35,785 kilometres (22,236 mi)[2] |
Apogee | 35,801 kilometres (22,246 mi)[2] |
Inclination | 0.03 degrees[2] |
Period | 1436.12 minutes[2] |
Epoch | 23 January 2015, 08:32:36 UTC[2] |
Transponders | |
Band | Ku band [3] |
Capacity | 32 Ku Transponders [3] |
Coverage area | CONUS[3] |
EIRP | 40.5 - 52.5 (varies by transponder and latitude) [4] [3] |
Nimiq 5 is a Canadian communications satellite, operated by Telesat Canada as part of its Nimiq fleet of satellites.[5] It is positioned in geostationary orbit at a longitude of 72.7° West of the Greenwich Meridian.[6] As of July 2015, EchoStar Corporation leases the satellite's entire capacity to provide High Definition television direct-to-home broadcasting for Dish Network Corporation.[6][4] When accessed using a multi-satellite receiver such as the VIP722k and a multi-satellite dish/LNB combo, such as the Dish-300, Dish-500, or Dish-Turbo 1000.4, the satellite is (incorrectly) referred to by the on-screen diagnostics as Echostar 72W.[citation needed]
Nimiq 5 was built by Space Systems/Loral, and is based on the LS-1300 satellite bus.[7] The contract to build it was announced on 4 January 2007.[8] At launch, it will have a mass of 4,745 kilograms (10,461 lb),[9] and is expected to operate for fifteen years. It carries 32 J band transponders (NATO frequency designation system, US IEEE Ku band).[7]
Nimiq 5 was launched by International Launch Services, using a Proton-M rocket with a Briz-M upper stage, under a contract signed in April 2007.[10] The launch was conducted from Site 200/39 at the Baikonur Cosmodrome in Kazakhstan, at 19:19 GMT on 17 September 2009. The Briz-M separated from the Proton-M nine minutes and forty one seconds into the flight and subsequently made five burns before releasing Nimiq 5 into a geosynchronous transfer orbit nine hours and fifteen minutes after liftoff.[9]
See also
References
<templatestyles src="Reflist/styles.css" />
Cite error: Invalid <references>
tag; parameter "group" is allowed only.
<references />
, or <references group="..." />
- ↑ Lua error in package.lua at line 80: module 'strict' not found.
- ↑ 2.0 2.1 2.2 2.3 2.4 Lua error in package.lua at line 80: module 'strict' not found.
- ↑ 3.0 3.1 3.2 3.3 Lua error in package.lua at line 80: module 'strict' not found.
- ↑ 4.0 4.1 Lua error in package.lua at line 80: module 'strict' not found.
- ↑ Lua error in package.lua at line 80: module 'strict' not found.
- ↑ 6.0 6.1 Lua error in package.lua at line 80: module 'strict' not found.
- ↑ 7.0 7.1 Lua error in package.lua at line 80: module 'strict' not found.
- ↑ Lua error in package.lua at line 80: module 'strict' not found.
- ↑ 9.0 9.1 Lua error in package.lua at line 80: module 'strict' not found.
- ↑ Lua error in package.lua at line 80: module 'strict' not found.