| Mission type | Communication |
|---|---|
| Operator | EchoStar |
| COSPAR ID | 2012-035A |
| SATCAT no. | 38551 |
| Mission duration | Planned: 15 years Elapsed: 11 years, 8 months, 22 days |
| 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 altitude | 35,781 kilometers (22,233 mi)[1] |
| Apogee altitude | 35,804 kilometers (22,248 mi)[1] |
| Inclination | 0.01 degrees[1] |
| Period | 1436.10 minutes[1] |
| Epoch | 25 January 2015, 05:22:59 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 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,[3] from where it is used for satellite internet access over HughesNet.[4]
EchoStar XVII was built by Space Systems/Loral,[5] and is based on 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 generates 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 is 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 used its own propulsion system to manoeuvre into a geostationary orbit.[4]
Path to geostationary orbit
EchoStar XVII · Earth
See also
- ViaSat-1 – Similar high throughput satellite that was the source of a lawsuit to the manufacturer of both
- 2012 in spaceflight
References
- ^ a b c d e "ECHOSTAR 17 Satellite details 2012-035A NORAD 38551". N2YO. 25 January 2015. Retrieved 25 January 2015.
- ^ a b c Krebs, Gunter. "Echostar 17 / Jupiter 1". Gunter's Space Page. Retrieved 9 July 2012.
- ^ a b c d "A Dual Launch for Internet and Weather Satellites" (PDF). Arianespace. Archived from the original (PDF) on 16 July 2012. Retrieved 9 July 2012.
- ^ a b "Hughes EchoStar XVII Satellite with JUPITER™ High Throughput Technology Successfully Launched". EchoStar. 6 July 2012. Archived from the original on 19 December 2014. Retrieved 8 July 2012.
- ^ "EchoStar XVII". Space Systems/Loral. Archived from the original on 18 June 2012. Retrieved 8 July 2012.
- ^ Bergin, Chris (5 July 2012). "Ariane 5 ECA launches with MSG-3 and EchoStar XVII". NASASpaceflight.com. Retrieved 9 July 2012.
This page was last edited on 27 February 2023, at 13:09