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astronautix.com AS 2100

AS 2100 satellite
AS 2100 satellite -

Credit: Lockheed-Martin. 22,265 bytes. 334 x 394 pixels.



Class: Communications. Nation: USA. Agency: Americom. Manufacturer: Lockheed-Martin.

Cost per satellite $100 million for the spacecraft including ground support equipment, but not including launch costs. 3-axis stabilised. Two large solar arrays. 18 operational C-Band channels with 45 W amplifiers.16 Ku-Band channels with 85 W amplifiers.4 Ku-Band channels at 135 watts.


Specification

Total Mass: 2,760 kg.


AS 2100 Chronology


08 September 1996 GE 1 Program: GE. Launch Site: Cape Canaveral . Launch Vehicle: Atlas IIA. Perigee: 35,780 km. Apogee: 35,793 km. Inclination: 0.0 deg.

Geostationary at 103.0W. Launch vehicle put payload into supersynchronous earth orbit with IFR/MRS trajectory option.


30 January 1997 GE 2 Program: GE. Launch Site: Kourou . Launch Vehicle: Ariane 44L. Perigee: 35,772 km. Apogee: 35,801 km. Inclination: 0.0 deg.

Geosynchronous. Stationed over 84.9W


04 September 1997 GE 3 Program: GE. Launch Site: Cape Canaveral . Launch Vehicle: Atlas IIAS. Perigee: 35,776 km. Apogee: 35,797 km. Inclination: 0.0 deg.

Geosynchronous. Stationed over 87.1W Launch vehicle put payload into supersynchronous earth orbit with IFR/MRS trajectory option.


07 May 1998 Echostar 4 Program: Echostar. Launch Site: Baikonur . Launch Vehicle: Proton 8K82K / DM3. Perigee: 35,781 km. Apogee: 35,790 km. Inclination: 0.0 deg.

Geostationary at 148.0 degrees W.


30 May 1998 Zhongwei 1 Program: Chinastar. Launch Site: Xichang . Launch Vehicle: CZ-3B. Perigee: 35,777 km. Apogee: 35,798 km. Inclination: 0.1 deg.

Also known as Chinastar 1; comsat to serve China, India, Korea and Southeast Asia with 18 C-band and 20 Ku-band transponders. Operated by the China Orient Telecommunications Satellite Company, part of the Chinese telecommunications ministry. Zhongwei 1 and the CZ-3B's final liquid hydrogen upper stage were placed in an initial supersynchronous 216 x 85,035 km x 24.4 deg transfer orbit. Geostationary at 87.6 degrees E.


20 May 1999 Nimiq 1 Program: Anik. Launch Site: Baikonur . Launch Vehicle: Proton 8K82K / DM3. Perigee: 35,785 km. Apogee: 35,787 km. Inclination: 0.0 deg.

Telesat Canada's Nimiq television broadcasting satellite was placed into a 7050 km x 35790 km x 15.9 degree transfer orbit. The Nimiq was to use its liquid apogee engine (Royal Ordnance Leros 1) to reach geosynchronous orbit. Telesat Canada also operated the Anik Canadian domestic communications satellites, the first of which was launched in 1972.


12 August 1999 Telkom 1 Program: Palapa. Launch Site: Kourou . Launch Vehicle: Ariane 42P. Mass: 2,763 kg. Perigee: 35,781 km. Apogee: 35,794 km. Inclination: 0.1 deg.

The launch vehicle delivered its H-10-3 third stage and the Telkom 1 payload into a 221 km x 35687 km x 7.0 degree geosynchronous transfer orbit 21 minutes after launch. Telkom 1 was owned by PT Telkomunikasi of Indonesia and was a successor to the Palapa series of satellites. Mass of Telkom 1 was 1700 kg in geosynchronous orbit after its on-board engine made the apogee burn. Stationed at 108 deg E.



AS 2100 satelliteAS 2100 satellite

Credit: Lockheed-Martin. 10,103 bytes. 208 x 258 pixels.


04 September 1999 Koreasat 3 Launch Site: Kourou . Launch Vehicle: Ariane 42P. Perigee: 35,786 km. Apogee: 35,789 km. Inclination: 0.0 deg.

Geosynchronous communications satellite. Stationed at 112 deg E.


13 November 1999 GE 4 Launch Site: Kourou . Launch Vehicle: Ariane 44LP. Perigee: 35,759 km. Apogee: 35,801 km. Inclination: 0.0 deg.

Provided C and Ku-band communications services for GE Americom, replacing Spacenet 4. Stationed at 101 deg W.


12 February 2000 Garuda 1 Launch Site: Baikonur . Launch Vehicle: Proton 8K82K / DM3. Perigee: 35,769 km. Apogee: 35,807 km. Inclination: 2.4 deg.

Geosynchronous communications satellite for the ACES consortium (PSN of Indonesia, PLDT of the Phillipines, Lockheed Martin, and Jasmine of Thailand). The satellite had two large 12-m diameter L-band antennae for cellular telephone relay. Stationed at 123 deg E.


14 September 2000 GE 7 Launch Site: Kourou . Launch Vehicle: Ariane 5. Perigee: 35,783 km. Apogee: 35,789 km. Inclination: 0.0 deg.

GE Americom satellite to provide cable TV distribution coverage to the USA. Equipped with 24 C-band transponders. Its dry mass was 912 kg and it carried 1023 kg of fuel at launch. The satellite is an A2100A model built by Lockheed Martin/Sunnyvale, the first lightweight A2100 with a mass about half that of earlier A2100 satellites. By September 19 GE 7 was in a 35,832 x 35,869 km x 0.1 deg orbit drifting over 146 deg W. Stationed at 137 deg W.


01 October 2000 GE-1A Launch Site: Baikonur . Launch Vehicle: Proton 8K82K / DM3. Perigee: 35,777 km. Apogee: 35,795 km. Inclination: 0.1 deg.

Ku-band communications satellite to provide broadcast services for eastern Asia. Stationed at 108 deg E.


06 October 2000 N-SAT-110 Launch Site: Kourou . Launch Vehicle: Ariane 42L. Perigee: 35,780 km. Apogee: 35,793 km. Inclination: 0.0 deg.

N-SAT-110, also known as Superbird 5, was jointly owned by SCC (Space Communications Corporation of Tokyo) and JSat (Japan Satellite Systems). SCC controlled the vehicle on orbit. The satellite carried 24 Ku-band transponders. By October 15 N-SAT-110 was in a 35610 x 35752 km x 0.1 deg orbit drifting past 109 deg E. Stationed at 110 deg E.



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Last update 12 March 2001.
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