Mission typeGeodesy
COSPAR ID1975-027A
SATCAT no.7734
Spacecraft properties
Spacecraft typeGEOS
ManufacturerJHU / APL
Launch mass346 kilograms (763 lb)
Dimensions1.32 by 0.81 meters (4.3 ft × 2.7 ft)
6 meters (20 ft) long with boom deployed
Start of mission
Launch date9 April 1975, 23:58:02 (1975-04-09UTC23:58:02Z) UTC[1]
RocketDelta 1410
Launch siteVandenberg SLC-2W
End of mission
DeactivatedJuly 1979
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Semi-major axis7,208.68 kilometers (4,479.27 mi)
Perigee altitude828 kilometers (514 mi)
Apogee altitude846 kilometers (526 mi)
Inclination114.98 degrees
Period101.52 minutes
Epoch14 January 2014, 03:51:02 UTC[2]
  • Radar altimeter (ALT)
  • Retroreflector array (RRA)
  • Doppler beacon
  • S-band antenna
  • C-band antenna (Two)
  • SST Tracking

GEOS-3, or Geodynamics Experimental Ocean Satellite 3, or GEOS-C, was the third and final satellite as part of NASA's Geodetic Earth Orbiting Satellite/Geodynamics Experimental Ocean Satellite program (NGSP)[3] to better understand and test satellite tracking systems.[4] For GEOS missions 1 and 2, GEOS stands for Geodetic Earth Orbiting Satellite; this was changed to Geodynamics Experimental Ocean Satellite for GEOS-3.[4]


The satellite mission was designed to further an understanding of the earth's gravitational field, size and shape of the terrestrial geoid, deep ocean tides, sea state, current structure, crustal structure, solid earth dynamics, and remote sensing technology.[5] Jerome Rosenburg at NASA Headquarters initiated the GEOS-3 project in 1970.[5] The project was to serve as a stepping stone between the GEOS program and the emerging NASA Earth and Ocean Physics Application Program.[5] GEOS-1 and GEOS-2 had provided useful information about the structure of the earth's gravitational field, but new technology was deemed necessary to gain a further understanding.[5] The project was initially cancelled due to budgetary concerns after an initial 1-year study, but was re-instated in late 1971.[5] The satellite was launched on April 9, 1975 and remained operational until late July 1979.[6]


The following is a list of instruments/systems that were on board or part of the GEOS-3 satellite, including a description of their general purpose:[5][7]

  • Radar Altimeter (ALT) – A multimode radar system with the ability to provide precise satellite-to-ocean surface height measurements. The radar system provided global and intensive data gathering modes, which could provide height precision measurements at 50 cm and 20 cm respectively.
  • Retroreflector Array (RRA) – An array of retroreflectors. These allow a ground-based laser to provide range information.
  • Doppler System – A system of dual frequency space borne doppler beacons at 162 and 324 MHz and a ground-based receiver station. This system was used to measure the effects of first-order ionospheric refraction and make corrections to the Doppler frequency.
  • S-band Tracking System – A tracking system which had three modes of operations for satellite to satellite tracking, ground-station tracking, and direct unified S-band.
  • C-band System – A system of two C-band radar transponders used to better understand the accuracies of the gravimetric and geometric measurements. The system also supported the altimeter and C-band calibration.
  • Satellite-to-Satellite Tracking (SST) – The SST experiment consisted of, the ground-based ATS ranging system, the wideband communication transponder on the ATS-6 geosynchronous spacecraft, and the ranging transponder on the LEO satellite.

Impacts on the scientific community

The GEOS-3 mission provided data that furthered scientific understanding in various fields. The ocean height data set from this mission provided the first comprehensive coverage in most areas of the world's oceans, providing a better understanding of the Ocean Geoid.[5] Ocean height also provided information about quasi-stationary departures from the geoid, for events like currents, eddies, storm surges, etc.[5] The return waveform data was used to better understand the sea state at a level that was comparable to buoy-collected data.[5] An unexpected result was the ability to use waveform data to derive surface wind speed, and the ability to maintain track over terrain and ice[5] Altimeter data from GEOS-3 has been utilized by many gravity models, including GEM-T3, JGM-1 and JGM-2 [6]


  1. ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 14 January 2014. CS1 maint: discouraged parameter (link)
  2. ^ "GEOS 3 Satellite details 1975-027A NORAD 7734". N2YO. 14 January 2014. Retrieved 14 January 2014. CS1 maint: discouraged parameter (link)
  3. ^ Henriksen, S. W. (ed) (1977) National Geodetic Satellite Program, NASA SP-365
  4. ^ a b "NASA – GEOS Program". eoPortal Directory. Retrieved 8 December 2013. CS1 maint: discouraged parameter (link)
  5. ^ a b c d e f g h i j Stanley, H. R. (30 July 1979). "The GEOS 3 Project". Journal of Geophysical Research. 84 (B8): 3779–3783. Bibcode:1979JGR....84.3779S. doi:10.1029/JB084iB08p03779.
  6. ^ a b "GEOS-3". JPL. Retrieved 8 December 2013. CS1 maint: discouraged parameter (link)
  7. ^ "GEOS 3". International Laser Ranging Service. Retrieved 8 December 2013. CS1 maint: discouraged parameter (link)