To accomplish these objectives, the spacecraft was equipped with (1) a three-camera return beam vidicon (RBV) to obtain visible light and near infrared photographic images of Earth, (2) a four-channel multispectral scanner (MSS) to obtain radiometric images of Earth, and (3) a data collection system (DCS) to collect information from remote, individually equipped ground stations and to relay the data to central acquisition stations. Landsat 1 carried two wide-band video tape recorders (WBVTR) capable of storing up to 30 min of scanner or camera data to give the spacecraft's sensors a near-global coverage capability.
An advanced attitude control system consisting of horizon scanners, sun sensors, and a command antenna combined with a freon gas propulsion system permitted the spacecraft's orientation to be maintained within plus or minus 0.7 degrees in all three axes. Spacecraft communications included a command subsystem operating at 154.2 and 2106.4 MHz and a PCM narrow-band telemetry subsystem, operating at 2287.5 and 137.86 MHz, for spacecraft housekeeping, attitude, and sensor performance data. Video data from the three-camera RBV system was transmitted in both real-time and tape-recorder modes at 2265.5 MHz, while information from the MSS was constrained to a 20-MHz rf bandwidth at 2229.5 MHz.
The spacecraft was turned off on January 6, 1978, when cumulative precession of the orbital plane caused the spacecraft to see almost constant sunlight which led to overheating.