GOES 6

Last updated
GOES-6
GOES 4-5-6-7 illustration.jpg
Artist's impression of an HS-371 derived GOES satellite
Mission type Weather satellite
Operator NOAA  / NASA
COSPAR ID 1983-041A OOjs UI icon edit-ltr-progressive.svg
SATCAT no. 14050
Mission duration7 years (planned)
6 years (VISSR)
9 years (achieved)
Spacecraft properties
Bus HS-371
Manufacturer Hughes
Launch mass660 kilograms (1,460 lb)
Start of mission
Launch date28 April 1983, 22:26 (1983-04-28UTC22:26Z) UTC
Rocket Delta 3914
Launch site Cape Canaveral LC-17A
Contractor McDonnell Douglas
End of mission
DisposalDecommissioned
Deactivated19 May 1992 (1992-05-20)
Orbital parameters
Reference system Geocentric
Regime Geostationary
Longitude135° West (1983-1984)
97° West (1984)
108° West (1984-1987)
135° West (1987-1992)
SlotGOES-WEST (1983-1984,1987-1992)
Semi-major axis 42,151.0 kilometers (26,191.4 mi)
Perigee altitude 35,759.4 kilometers (22,219.9 mi)
Apogee altitude 35,800.9 kilometers (22,245.6 mi)
Inclination 14.7°
Period 1,435.1 minutes
 

GOES-6, known as GOES-F before becoming operational, was a geostationary weather satellite which was operated by the United States National Oceanic and Atmospheric Administration as part of the Geostationary Operational Environmental Satellite system. [1] Launched in 1983, it was used for weather forecasting in the United States.

Contents

GOES-6 was built by Hughes Space and Communications, and was based on the HS-371 satellite bus. At launch it had a mass of 660 kilograms (1,460 lb), [2] with an expected operational lifespan of around seven years.

Launch

GOES-F was launched using a Delta 3914 carrier rocket [3] flying from Launch Complex 17A at the Cape Canaveral Air Force Station. [4] The launch occurred at 22:26 GMT on 28 April 1983. [5]

Orbit

The launch successfully placed GOES-F into a geosynchronous transfer orbit, from which it raised itself to geostationary orbit by means of an onboard Star 27 apogee motor, with insertion occurring on 9 May 1983. [6]

Following insertion into geosynchronous orbit, GOES-6 was positioned at 135° West. In 1984 it was moved, initially to 97° West, and later to 108° West to cover for the failure of the Visible Infrared Spin-Scan Radiometer on GOES-5. After GOES-7 replaced GOES-5 in 1987, GOES-6 was returned to 135° West, where it remained for the rest of its operational life. [4] Its imager had failed on 21 January 1989, [1] leaving GOES-7 as the only operational GOES satellite for over five years, until the launch of GOES-8 in 1994. Following this failure, it remained operational as a relay satellite until it was retired to a graveyard orbit on 19 May 1992. [1] [6]

Launch of GOES-F on a Delta 3914 Launch of GOES-F Spac0253.jpg
Launch of GOES-F on a Delta 3914

See also

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References

  1. 1 2 3 "GOES-6". The GOES Program - ESE 40th Anniversary. NASA. Archived from the original on 2006-10-04. Retrieved 2009-08-15.
  2. "GOES-6". NSSDC Master Catalog. US National Space Science Data Center. Retrieved 2009-08-15.
  3. Krebs, Gunter. "GOES 4, 5, 6, G, 7". Gunter's Space Page. Retrieved 2009-08-15.
  4. 1 2 Wade, Mark. "GOES". Encyclopedia Astronautica. Archived from the original on February 21, 2002. Retrieved 2009-08-15.
  5. McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 2009-08-15.
  6. 1 2 McDowell, Jonathan. "Index". Geostationary Orbit Catalog. Jonathan's Space Page. Archived from the original on 2010-04-06. Retrieved 2009-08-15.