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Satellite Data System
American military satellite communication system

The Satellite Data System (SDS) is a system of United States military communications satellites. At least three generations have been used: SDS-1 from 1976 to 1987; SDS-2 from 1989 to 1996; SDS-3 from 1998 to the present. It is believed that these satellites were known by the code name Quasar. The first generation was named simply 'SDS', the second generation was named 'Quasar' and the third generation each had their own designations.

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Orbital characteristics

SDS satellites have a highly elliptical orbit, going from about 300 kilometers at perigee to roughly 39,000 km at apogee in order to allow communications with polar stations that cannot contact geosynchronous satellites. The high apogee meant that the polar regions were visible for long amounts of time, and only two satellites were required in order to achieve constant communications ability. In addition, two geostationary satellites appear to be part of the system. The SDS satellites were constructed by Hughes Aircraft Company.

Mission

The primary purpose of the SDS satellites is to relay imagery from low-flying reconnaissance satellites, notably the Keyhole optical reconnaissance and Lacrosse/Onyx radar reconnaissance satellites to ground stations in the United States.3

SDS-1

Each SDS-1 satellite had 12 channels available for Ultra high frequency (UHF) communication. They were cylindrical in shape, roughly 25 ft (7.6 m) long. 980 watts of electrical power were available from solar panels and batteries. The SDS-1 had a mass of 630 kg (1,390 lb) and was launched on Titan-3B rockets. The SDS-1 satellites had similar orbits to the Air Force's Jumpseat ELINT satellites.4

It has been speculated that the early satellites served as data relays for the first KH-11 Kennen reconnaissance satellites.5

SDS-2

The SDS-2 is significantly more massive at 2,335 kg (5,148 lb), with three separate communication dishes, including one for a K-band downlink. Two dishes are 4.5 m (15 ft) in diameter, while the third is 2 m (6 ft 7 in) in diameter. The solar arrays generate 1238 watts of power. It is believed that the Space Shuttle has been used to launch several satellites, possibly on missions STS-28, STS-38, and STS-53. Other launches have used the Titan IV launch vehicle.

Satellites

NameCOSPAR ID6SATCAT №Launch dateLaunch vehicleLaunch siteLaunch designationPerigeeApogeeInclinationRemarks

First generation

OPS 78371976-050A088712 June 1976Titan III(34)BVAFB, SLC-4WSDS F-1380 km39315 km63.3 deg
OPS 79401976-080A092706 August 1976Titan III(34)BVAFB, SLC-4WSDS F-2380 km39315 km63.3 deg
OPS 73101978-075A109935 August 1978Titan III(34)BVAFB, SLC-4WSDS F-3380 km39315 km63.3 deg
OPS 58051980-100A1209313 December 1980Titan III(34)BVAFB, SLC-4W
USA-41984-091A1522628 August 1984Titan III(34)BVAFB, SLC-4WSDS F-5A
USA-9195-014A155468 February 1985Titan III(34)BVAFB, SLC-4WUSA-9
USA-211987-015A1750615 February 1987Titan III(34)BVAFB, SLC-4WSDS F-6

Second generation

USA-401989-061B201672 June 1989Space Shuttle ColumbiaSTS-28/Orbus-21SKSC, LC-39BN/A
USA-671990-097B2096315 November 1990Space Shuttle AtlantisSTS-38/Orbus-21SKSC, LC-39AGeosynchronous satellite, deployed along with Prowler and initially misidentified as a Magnum SIGINT spacecraft
USA-891992-086B225182 December 1992Space Shuttle DiscoverySTS-53/Orbus-21SKSC, LC-39A
USA-1251996-038A239453 July 1996Titan IV(405)ACCAFS, LC-40

Third generation

USA-1371998-005A2514829 January 1998Atlas IIACCAFS, SLC-36ANROL-5Capricorn, Molniya orbit
USA-1552000-080A266356 December 2000Atlas IIASCCAFS, SLC-36ANROL-10Great Bear, geosynchronous satellite at 10° West
USA-1622001-046A2694811 October 2001Atlas IIASCCAFS, SLC-36BNROL-12Aquila, geosynchronous satellite at 144° West
USA-1792004-034A2838431 August 2004Atlas IIASCCAFS, SLC-36ANROL-1Nemesis, Molniya orbit, final Atlas II launch
USA-1982007-060A3237810 December 2007Atlas V 401CCAFS, SLC-41NROL-24Scorpius, Molniya orbit
USA-2272011-011A3737711 March 2011Delta IV-M+(4,2)CCAFS, SLC-37BNROL-27Gryphon, geosynchronous satellite at 10° West, replaced USA-155
USA-2362012-033A3846620 June 2012Atlas V 401CCAFS, SLC-41NROL-38Drake, geosynchronous satellite at 144° West, replacement for USA-162
USA-2522014-027A3975122 May 2014Atlas V 401CCAFS, SLC-41NROL-33Geosynchronous satellite
USA-2692016-047A4172428 July 2016Atlas V 421CCAFS SLC-41NROL-61Spike, Geosynchronous orbit, might be a new generation 7
USA-2792017-066A4297315 October 2017Atlas V 421CCAFS, SLC-41NROL-52Likely Geosynchronous orbit8
  • Spaceflight portal

References

  1. Jonathan's Space Report: NRO Satellite Names http://planet4589.org/nro/nro.html

  2. Jonathan's Space Report: Satellite Catalogue http://planet4589.org/space/log/satcat.txt

  3. Richelson, J.T. (2001). The Wizards of Langley. Inside the CIA's Directorate of Science and Technology. Boulder, Colorado: Westview Press. ISBN 9780813340593. 9780813340593

  4. National Reconnaissance Office: "NRO Brochure circa 1997"[permanent dead link] http://www.zianet.com/jpage/black/NRO%20Brochure.pdf

  5. Day, Dwayne A. (26 February 2018). "Shadow dancing: the Satellite Data System". The Space Review. http://www.thespacereview.com/article/3440/1

  6. Jonathan's Space Report: List of satellite launches http://planet4589.org/space/log/

  7. "NROL-61 satellite launched Thursday spotted in space by sky-watchers". Spaceflight Now. 30 July 2016. https://spaceflightnow.com/2016/07/30/nrol-61-satellite-launched-thursday-spotted-in-space-by-sky-watchers/

  8. Graham, William (15 October 2017). "Atlas V finally launches with NROL-52". NASASpaceFlight.com. Retrieved 15 October 2017. https://www.nasaspaceflight.com/2017/10/ula-atlas-v-nrol-52-launch-cape-canaveral/