EchoStar XVII
| Mission type | Communication |
|---|---|
| Operator | EchoStar |
| COSPAR ID | 2012-035A |
| SATCAT no. | 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 UTC |
| Rocket | Ariane 5ECA |
| Launch site | Kourou ELA-3 |
| Contractor | Arianespace |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Geostationary |
| Longitude | 107.1° West |
| Perigee | 35,781 kilometers (22,233 mi) |
| Apogee | 35,804 kilometers (22,248 mi) |
| Inclination | 0.01 degrees |
| Period | 1436.10 minutes |
| Epoch | 25 January 2015, 05:22:59 UTC |
| Transponders | |
| Band | 60 Ka band (NATO K band) |
EchoStar XVII or EchoStar 17, also known as Jupiter 1, is an American geostationary high throughput communications satellite which is operated by Hughes Network Systems, a subsidiary of EchoStar. It is positioned in geostationary orbit at a longitude of 107.1° West, from where it is used for satellite internet access over HughesNet.
EchoStar XVII was built by Space Systems/Loral, and is based on the LS-1300 satellite bus. 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 generates a minimum of 16.1 kilowatts of power. The spacecraft had a mass at liftoff of 6,100 kilograms (13,400 lb), and is expected to operate for fifteen years. It carries sixty Ka band (NATO K band) transponders which is used to cover North America.
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. The MSG-3 weather satellite was launched aboard the same rocket, mounted below EchoStar XVII, which was atop a Sylda 5 adaptor. The launch successfully placed both satellites into a geosynchronous transfer orbit. EchoStar XVII used its own propulsion system to manoeuvre into a geostationary orbit.
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