National Oceanic and Atmospheric Administration (NOAA)
Earth Observation Satellite Company (EOSAT)
Department of the Interior (DOI) U.S. Geological Survey (USGS)
Launch
Date: July 16, 1982
Vehicle: Delta 3920
Launched by: NASA
Site: Vandenberg Air Force Base, California
Spacecraft
3-axis stabilized, zero momentum with control of 0.01 deg using reaction wheels
Aluminum with graphite struts
Hydrazine propulsion system
Single solar array with 1-axis articulation
Three Nickel Cadmium (NiCd) batteries provide 100 Ampere-Hour (AHr ) total
Retractable boom (4 m long) with 2 powered joints supports the articulated High Gain Antenna, which downlinked data via the Tracking and Data Relay Satellite System (TDRSS)
Weight: approximately 4,300 lbs (1,942 kg)
Communications
Direct downlink with TDRSS
Data rate: 85 Mbps
Communications system uses S, X, L, and Ku Bands
Quantization: 8 bit (256 levels)
Orbit
Worldwide References System-2 (WRS-2) path/row system
Circular, sun-synchronous, near-polar orbit at an altitude of 705 km (438 mi)