EchoStar I
OperatorEchoStar
Cospar id1995-073A
Satcat23754
Mission duration12 years
Spacecraft busAS-7000
ManufacturerLockheed Martin Astro Space
Launch mass3,287 kilograms (7,247 lb)
Dimensions4.08 × 2.22 × 2.54 m (13.4 × 7.3 × 8.3 ft)
Power5 kW
Launch dateDecember 28, 1995, 11:50 UTC
Launch rocketLong March 2E EPKM
Launch siteXichang LC-2
Orbit epochMay 14, 2017
Orbit referenceGeocentric
Orbit regimeGeostationary
Orbit periapsis35,780.7 kilometers (22,233.1 mi)
Orbit apoapsis35,806.7 kilometers (22,249.3 mi)
Orbit inclination0.7 degrees
Orbit semimajor42,164.0 kilometers (26,199.5 mi)
Orbit period1,436.1 minutes
Orbit longitude77° West
Apsisgee
Trans band16
Trans coverageContiguous United States
Trans eirp53 dBW

EchoStar I was 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. It appears to be retired as of 2023.

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-metre (1.6-foot) 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. ^ TSE. "EchoStar 1". Retrieved May 14, 2017.