Landsat Diagrams and Technical Illustrations
This gallery includes Landsat technical illustrations, diagrams, sensor schematics, and orbital visualizations.
This gallery includes Landsat technical illustrations, diagrams, sensor schematics, and orbital visualizations.















![This schematic appears in The Landsat Tutorial Workbook: Basics of Satellite Remote Sensing, written by Dr. Nicholas Short and published by the NASA Scientific and Technical Information Branch in 1982. Dr. Short writes, “The Landsat-1 spacecraft was launched on July 23, 1972, and positioned in the orbit shown in [this figure]. Landsat-2 was launched on June 22, 1975, and Landsat-3 was launched on March 5, 1978. “These satellites [had] a nominal altitude of 917 km (570 miles); 99° orbital inclination, which makes them nearly polar; and a sun-synchronous orbit, which means that the orbit plane precesses about the Earth at the same angular rate that the Earth moves about the Sun. This feature enables the spacecraft to cross the Equator at the same local time (about 9:30 to 10:00 a.m.) on the sunlit side of the Earth.”](https://assets.science.nasa.gov/dynamicimage/assets/science/missions/landsat/landsat-1-3-mission-pages/T044623.png?w=600&h=431&fit=clip&crop=faces%2Cfocalpoint)


![This schematic appears in the ERTS Reference Manual that was prepared by General Electric prior to the Landsat 1 (ERTS-1) launch in 1972. The schematic shows the Landsat 1 flight profile, from liftoff (0) to spacecraft separation (10). The manual tells us, “an all-inertial guidance system, consisting of an inertial sensor package and guidance computer, controls the vehicle and sequence of operations from liftoff to spacecraft separation. The flight profile is presented in [this figure] .”](https://assets.science.nasa.gov/dynamicimage/assets/science/missions/landsat/2020/07/launch.jpg?w=1152&h=1152&fit=clip&crop=faces%2Cfocalpoint)










![Like all of the Landsat satellites, Landsat-6 would have been in a sunscreen orbit had its launch been successful. The L6 Handbook tells us, “Establishment of the sun-synchronous orbit provides for minimal variation of solar illuminations at the spacecraft and at the observed Earth scene. This occurs because of the near constancy of the geometry between the orbit plane and the sun vector. By achieving the correct combinations of altitude and orbit inclination, the orbit will precess about the geographic North Pole in the same direction (west to east) and at the same annual rate as the apparent Sun’s motion relative to the Earth. The geometry of the orbit-Earth-Sun relationship by season is shown in [this figure]. This figure also indicates how ground scene illumination is affected by changes in season. Such seasonal variations also have an impact on illumination at the spacecraft.”](https://assets.science.nasa.gov/dynamicimage/assets/science/missions/landsat/landsat-1-3-mission-pages/seasons-1024x1024.png?w=1024&h=1024&fit=clip&crop=faces%2Cfocalpoint)








