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U.S. Navy Earth observation satellite

Geosat

Geosat
All data from the card 24
Mission type
Earth science
Operator
United States Navy
COSPAR ID
1985-021A
SATCAT no.
15595
Mission duration
5 Years
Dry mass
635.0 kilograms (1,399.9 lb)
Launch date
March 13, 1985, 02:00 UTC
Rocket
Atlas E OIS
Launch site
Vandenberg SLC-3W
Deactivated
January 1990
Reference system
Geocentric
Regime
LEO
Semi-major axis
7,146.2 kilometres (4,440.4 mi)
Eccentricity
0.00398
Perigee altitude
757 kilometres (470 mi)
Apogee altitude
814 kilometres (506 mi)
Inclination
108.0596 degrees
Period
100.6 minutes
RAAN
309.0682 degrees
Argument of perigee
276.8275 degrees
Mean anomaly
131.8715 degrees
Mean motion
14.37442186
Epoch
9 December 2013
Revolution no.
50565

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
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
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.

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