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Geosat

U.S. Navy Earth observation satellite

Geosat

U.S. Navy Earth observation satellite

FieldValue
nameGeosat
imageGeosat.jpg
image_captionArtist's interpretation of the Geosat satellite
mission_typeEarth science
operatorUnited States Navy
COSPAR_ID1985-021A
SATCAT15595
mission_duration5 Years
dry_mass635.0 kg
launch_dateUTC
launch_rocketAtlas E OIS
launch_siteVandenberg SLC-3W
deactivatedJanuary 1990
last_contact
orbit_epoch9 December 2013
orbit_referenceGeocentric
orbit_regimeLEO
orbit_periapsis757 km
orbit_apoapsis814 km
orbit_eccentricity0.00398
orbit_semimajor7146.2 km
orbit_inclination108.0596 degrees
orbit_period100.6 minutes
orbit_RAAN309.0682 degrees
orbit_arg_periapsis276.8275 degrees
orbit_mean_anomaly131.8715 degrees
orbit_mean_motion14.37442186
orbit_rev_number50565
apsisgee

The GEOSAT (GEOdetic SATellite) was a U.S. Navy Earth observation satellite, launched on March 12, 1985 into an 800 km, 108° inclination orbit, with a nodal period of about 6040 seconds. The satellite carried a radar altimeter capable of measuring the distance from the satellite to sea surface with a relative precision of about 5 cm. Its 18-month initial phase was a classified Geodetic Mission with a near-23-day repeat that was intended to replicate the orbit of the short-lived Seasat. After this, the satellite was maneuvered into a near-17-day exact repeat for oceanographic research.

Mission

Atlas-E OIS (41E) launching Geosat

The Geosat Geodetic Mission goal was to provide information on the marine gravity field. If the ocean surface were at rest, and no forces such as tides or winds were acting on it, the water surface would lie along the geoid. To first order, the Earth shape is an oblate spheroid. Subsurface features such as seamounts create a gravitational pull, and features such as ocean trenches create lower gravity areas. Spatial variations in gravity exert influence on the ocean surface and thereby cause spatial structure in the geoid. The deviations of the geoid from the first order spheroid are on the order of ± 100m. By measuring the position of the water surface above the Earth center, the geoid is observed, and the gravity field can be computed through inverse calculations.

Exact Repeat Mission

After the Geodetic Mission (GM) concluded 30 September 1986, GEOSAT's scientific Exact Repeat Mission (ERM) began on November 8, 1986 after being maneuvered into a 17.05 day, 244 pass exact repeat orbit that was more favorable for oceanographic applications. When the ERM ended in January 1990, due to failure of the two on-board tape recorders, more than three years of ERM data were collected and made available to the scientific community.

Once the GM goal had been reached, the satellite still had a useful life. An opportunity existed to observe the next order physical process that affects the ocean surface. Currents, tides and wind forcing all create changes in water levels. While there are extreme waves and events (tsunamis and hurricane surge), typical ocean features would be considered large if the water level change caused by them were 1 m. Most areas of the world experience features of typical amplitude of 20 cm. The ERM established the satellite in an exact repeat orbit. The satellite would orbit the Earth, and after 17.05 days the satellite would return to the same point. The satellite was actively controlled through thrust maneuvers to maintain the exact repeat orbit to within 1 km of the predefined ground track. In this manner, the satellite could observe long term changes at the points along the ground track.

Declassification

The U.S. Navy declassified parts of the Geodetic Mission data in 1990 that covered a doughnut-shaped area of ocean that surrounds Antarctica between 60 and 72 degrees south latitude. In 1992, further parts of the Geodetic Mission data over the oceans south of 30 degrees south were released. The GEOSAT data for the entire global sea surface was declassified in July 1995 after the competition of the geodetic phase of ESA ERS-1 mission. These data were subsequently widely used to estimate ocean bathymetry along with additional satellite altimeters.

GFO

GFO (Geosat Follow-On) Satellite

The successor to GEOSAT is the Geosat Follow-On (GFO) mission, launched 10 February 1998 by a Taurus rocket from Vandenberg AFB. GFO carried a water vapor radiometer as well as a radar altimeter, and operated in the same orbit as GEOSAT's Exact Repeat Mission. In addition, GFO carried a GPS receiver (which was never used operationally), Doppler receivers, and laser retro-reflectors for orbit determination. GFO was scheduled for retirement on December 31, 2008, but in late September 2008, the deteriorating state of the spacecraft resulted in a decision to accelerate the shutdown. Despite a series of system failures aboard the spacecraft, controllers were able to successfully lower GFO to a disposal orbit and shut it down on November 25, 2008. A successor mission, named GFO-2, was planned for launch in 2014, and would have featured a dual-band altimeter, instead of the single-band altimeter on the previous spacecraft. GFO-2 was cancelled by the U.S. Navy on 30 June 2010.

References

References

  1. Born, G.H.. (1987). "Design of the GEOSAT Exact Repeat Mission". APL-APL Tech. Dig..
  2. (1997). "Marine gravity anomaly from Geosat and ERS-1 satellite altimetry". J. Geophys. Res..
  3. "GFO - NSSDC ID: 1998-007A". NASA NSSDC.
  4. "The GFO Spacecraft and Mission Design". Computer Sciences Corporation.
  5. (2009). "GFO: Disposal of a Power-Challenged Satellite with an Attitude (Control) Problem".
  6. (April 19, 2010). "Ball Aerospace Wins Contract for Navy's GFO-2 Altimetry Satellite". Ball Aerospace.
  7. (16 March 2016). "Cancelled Department of the Navy Security Classification Guide Report".
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