EchoStar I

EchoStar I
Mission type Communications
Operator EchoStar
COSPAR ID 1995-073A
SATCAT no. 23754
Mission duration 12 years
Spacecraft properties
Bus AS-7000
Manufacturer Lockheed Martin Astro Space
Launch mass 3,287 kilograms (7,247 lb)
Dimensions 4.08 × 2.22 × 2.54 m (13.4 × 7.3 × 8.3 ft)
Power 5 kW
Start of mission
Launch date December 28, 1995, 11:50 (1995-12-28UTC11:50Z) UTC
Rocket Long March 2E EPKM
Launch site Xichang LC-2
Orbital parameters
Reference system Geocentric
Regime Geostationary
Longitude 77° West
Semi-major axis 42,164.0 kilometers (26,199.5 mi)
Perigee 35,780.7 kilometers (22,233.1 mi)
Apogee 35,806.7 kilometers (22,249.3 mi)
Inclination 0.7 degrees
Period 1,436.1 minutes
Epoch May 14, 2017
Transponders
Band 16 Ku band
Coverage area Contiguous United States
EIRP 53 dBW

EchoStar I is a communications satellite operated by EchoStar. Launched in 1995 it was operated in geostationary orbit at a longitude of 77 degrees west for 12 or 15 years. The company has approved the transfer of the 77 degree west orbital position to QuetzSat as of September 22, 2010.

Satellite

The launch of EchoStar made use of a Long March rocket flying from Xichang Satellite Launch Center in Sichuan province of the People's Republic of China. The launch took place at 11:50 UTC on December 28, 1995, 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 meter dishes on the ground in the American continents.[1][2]

Specifications

See also

References

  1. Krebs, Gunter. "EchoSatr 1, 2". Gunter's Space Page. Retrieved May 14, 2017.
  2. "EchoStar 1". Retrieved May 14, 2017. |first1= missing |last1= in Authors list (help)
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