Official name GOES 10
Alternative name GOES 10
Cospar ID 1997-019A
Norad ID 24786
Launch date 1997-04-25
Launch site AFETR
Launch vehicle Atlas-1
Country/Organization USA
Type application Meteorology
Operator NOAA
RCS size LARGE
Decay date ON ORBIT
Period (min) 1452.69
Inclination (deg) 12.21
Perigee (km) 35993
Apogee (km) 36229
Eccentricity 0.00326770236216111
Mean motion (revs. per day) 0.991264481754538
Semi-Major axis (km) 42489.135
Raan (deg) 26.3541
Arg of perigee (deg) 218.0259
Shape Box + 1 Pan + 1 Ant
Mass (kg) 1298.32
Height (m) 4.5
Width (m) 2.5
Depth (m) 2.5
Span (m^2) 26.9
Contractors Space Systems/Loral (SS/L)
Equipment ?
Propulsion R-4D-11
Configuration SSL-1300
Power Deployable solar array, batteries

Space Systems/Loral (SS/L) is designing and building a series of five meteorological and environmental satellites to provide scientists with vital data to forecast weather, identify and track severe local storm conditions, gather data for meteorological research, monitor solar activity, and relay signals from ships and aircraft in distress.

Named GOES (Geostationary Operational Environmental Satellite) I through M, the spacecraft are being built for NASA, as manager of the program for NOAA. The first GOES was launched in 1994 aboard an Atlas-1, the last was launched in 2001 on an Atlas-2A. The launches are staggered to keep two operational satellites on orbit at all times.

Three satellites are already on station, delivering data of such high quality that it has surprised and gratified the scientists that depend on its information. They provide 24-hour monitoring and measurement of dynamic weather events in real-time, and are the first to deliver simultaneous independent imaging and sounding from geostationary orbit. GOES provides the extremely accurate image navigation capability (within 2.1 miles) necessary to successfully track local area severe storms. Over the course of the contract, signed in late 1985, many design improvements have been made to improve spacecraft performance and to allow an increase in size. Such efforts continue. New instrumentation has been developed and added to the payload.

On-board instruments include a new-generation Imager that operates in both visible and infrared spectra, and a Sounder which continuously measures vertical temperature profiles. The Space Environment Monitor includes a magnetometer, energetic-particle sensor, highenergy proton and alpha-particle detector, and a solar X-ray sensor. The X-ray sensor regularly monitors solar flare activity that could cause high-level electron bombard-ment of people in space and satellites, affect the weather, and cause static.

The GOES spacecraft is based on SS/L's three-axis, bodystabilized FS-1300 bus.

GOES 9 failed in 1998 due to momentum wheel problems.

Satellite COSPAR Date LS Launch Vehicle Remarks
GOES 8 1994-022A 1994-04-13 AFETR Atlas-1
GOES 9 1995-025A 1995-05-23 AFETR Atlas-1
GOES 10 1997-019A 1997-04-25 AFETR Atlas-1
GOES 11 2000-022A 2000-05-03 AFETR Atlas-2A
GOES 12 2001-031A 2001-07-23 AFETR Atlas-2A