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EchoStar XVII

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Title: EchoStar XVII  
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Subject: 2012 in spaceflight, High throughput satellite, EchoStar, EchoStar XVI, Hughes Communications
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EchoStar XVII

EchoStar XVII
Mission type Communication
Operator EchoStar
COSPAR ID 2012-035A
SATCAT № 38551
Mission duration 15 years (planned)
Spacecraft properties
Bus LS-1300
Manufacturer Space Systems/Loral
Launch mass 6,100 kilograms (13,400 lb)
Start of mission
Launch date 5 July 2012, 21:36 (2012-07-05T21:36Z) UTC
Rocket Ariane 5ECA
Launch site Kourou ELA-3
Contractor Arianespace
Orbital parameters
Reference system Geocentric
Regime Geostationary
Longitude 107.1° West
Perigee 35,782 kilometers (22,234 mi)[1]
Apogee 35,802 kilometers (22,246 mi)[1]
Inclination 0.01 degrees[1]
Period 1436.09 minutes[1]
Epoch 30 November 2014, 06:01:16 UTC[1]
Transponders
Band 60 Ka band (NATO K band)

EchoStar XVII or EchoStar 17, also known as Jupiter 1,[2] is an American geostationary communications satellite which is operated by Hughes Network Systems, a subsidiary of EchoStar. It will be positioned in geostationary orbit at a longitude of 107.1° West,[3] from where it will be used for satellite broadband.[4]

EchoStar XVII was built by Space Systems/Loral,[5] and is based around the LS-1300 satellite bus.[2] It measures 8.0 metres (26.2 ft) by 3.2 metres (10 ft) by 3.1 metres (10 ft), with 26.07-meter (85.5 ft) solar arrays which were deployed after launch, and will generate a minimum of 16.1 kilowatts of power.[3] The spacecraft had a mass at liftoff of 6,100 kilograms (13,400 lb), and is expected to operate for fifteen years.[2] It carries sixty Ka band (NATO K band) transponders which will be used to cover North America.[3]

EchoStar XVII was launched by Arianespace, using an Ariane 5ECA carrier rocket flying from ELA-3 at Kourou. The spacecraft was launched at 21:36 UTC on 5 July 2012.[6] The MSG-3 weather satellite was launched aboard the same rocket, mounted below EchoStar XVII, which was atop a Sylda 5 adaptor.[3] The launch successfully placed both satellites into a geosynchronous transfer orbit. EchoStar XVII will use its own propulsion system to manoeuvre into a geostationary orbit.[4]

See also

References

  1. ^ a b c d e "ECHOSTAR 17 Satellite details 2012-035A NORAD 38551". N2YO. 30 November 2014. Retrieved 30 November 2014. 
  2. ^ a b c Krebs, Gunter. "Echostar 17 / Jupiter 1". Gunter's Space Page. Retrieved 9 July 2012. 
  3. ^ a b c d "A Dual Launch for Internet and Weather Satellites". Arianespace. Retrieved 9 July 2012. 
  4. ^ a b "Hughes EchoStar XVII Satellite with JUPITER™ High Throughput Technology Successfully Launched". EchoStar. 6 July 2012. Retrieved 8 July 2012. 
  5. ^ "EchoStar XVII". Space Systems/Loral. Retrieved 8 July 2012. 
  6. ^ Bergin, Chris (5 July 2012). "Ariane 5 ECA launches with MSG-3 and EchoStar XVII". NASASpaceflight.com. Retrieved 9 July 2012. 
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