EchoStar II
EchoStar II is a communications satellite operated by EchoStar. Launched in 1996 it was operated in geostationary orbit at a longitude of 148 degrees west for 12 or 15 years.
| Mission type | Communications | 
|---|---|
| Operator | EchoStar | 
| COSPAR ID | 1996-055A | 
| SATCAT no. | 24313 | 
| Mission duration | 12 years | 
| Spacecraft properties | |
| Bus | AS-7000 | 
| Manufacturer | Lockheed Martin | 
| Launch mass | 2,885 kg (6,360 lb) | 
| Dry mass | 2,000 kg (4,400 lb) | 
| Power | 7 kW | 
| Start of mission | |
| Launch date | September 11, 1996, 00:59 UTC | 
| Rocket | Ariane-42P H10-3 | 
| Launch site | Kourou ELA-2 | 
| End of mission | |
| Deactivated | July 14, 2008 | 
| Orbital parameters | |
| Reference system | Geocentric | 
| Regime | Geostationary | 
| Longitude | 80° West (current position)[1] | 
| Semi-major axis | 42,146.0 km (26,188.3 mi)[1] | 
| Perigee altitude | 35,764.4 km (22,223.0 mi)[1] | 
| Apogee altitude | 35,787.2 km (22,237.1 mi)[1] | 
| Inclination | 7.1 degrees[1] | 
| Period | 1,435.2 minutes[1] | 
| Epoch | November 28, 2017[1] | 
| Transponders | |
| Band | 16 Ku band | 
| Frequency | Uplink: 17.3 - 17.8 GHz Downlink: 12.2 - 12.7 GHz | 
| Bandwidth | 24 MHz | 
| Coverage area | Contiguous United States | 
| EIRP | 53 dBW | 
Satellite
    
The launch of EchoStar I made use of an Ariane 4 rocket flying from Guiana Space Centre in Kourou, French Guiana. The launch took place at 00:59 UTC on September 11, 1996,[2] with the spacecraft entering a geosynchronous transfer orbit. The spacecraft carried 16 Ku band transponders to enable direct broadcast communications and television channels through 0.5 metres (1 ft 8 in) dishes on the ground in the Contiguous United States.[3]
From September 1996 to November 2001, it was at position 118.8° W, while from December 2001 until July 2008, it was at position 148° W. The satellite ended its activities on July 14, 2008.
Specifications
    
- Launch mass: 2,885 kilograms (6,360 lb)
- Power source: 2 deployable solar arrays, batteries
- Stabilization: 3-axis
- Propulsion: 2 × LEROS-1B
See also
    
    
References
    
- N2yo. "ECHOSTAR 2". Retrieved November 28, 2017.
- NASA, Goddard Space Fight Center. "Echostar 2". Retrieved November 28, 2017.
- The Satellite Encyclopedia. "EchoStar 2". Retrieved November 28, 2017.