Intelsat K

Intelsat K
Mission type Communications
Operator Intelsat / SES World Skies
COSPAR ID 1992-032A
SATCAT no. 21989
Mission duration 10 years
Spacecraft properties
Bus AS-5000
Manufacturer Lockheed Martin
Launch mass 2,928 kilograms (6,455 lb)
Dry mass 2,836 kilograms (6,252 lb)
Start of mission
Launch date 10 June 1992, 00:00 (1992-06-10Z) UTC
Rocket Atlas-Centaur IIA
Launch site Cape Canaveral LC-36B
Orbital parameters
Reference system Geocentric
Regime Geostationary
Longitude 21.5° W
Semi-major axis 43,053.0 kilometers (26,751.9 mi)
Perigee 36,307.5 kilometers (22,560.4 mi)
Apogee 37,058.0 kilometers (23,026.8 mi)
Inclination 12°
Period 1,481.8 minutes
Epoch 19 April 2017
Transponders
Band 16 IEEE Ku band

Intelsat K (later termed Satcom K4 and NSS-K) was a geostationary communication satellite built by Lockheed Martin. It was located at orbital position of 21.5 degrees east longitude and was owned by SES World Skies. The satellite was based on the AS-5000 platform and its life expectancy was 10 years. He retired from service in August 2002 and was transferred to a graveyard orbit.

The satellite was purchased from Intelsat by New Skies and renamed to NSS-K. He is also the former Satom K4 of GE Americom. The satellite was successfully launched into space on June 10, 1992, by means of an Atlas-Centaur from the Cape Canaveral Air Force Station, United States. It had a launch mass of 2836 kg. It was equipped with 16 Ku band transponders.[1]

References

  1. Krebs, Gunter. Intelsat K /NSS K. Gunter's Space Page. Retrieved 2017-04-19.


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