Each Landmapper-BC spacecraft carries three separate cameras to gather 22 meter resolution imagery in the red, green, and
near-infrared spectral bands. The Landmapper-HD satellite design includes a larger telescope to gather 2.5 meter resolution imagery in blue, green, red,
red edge, and near-infrared spectral bands. This imagery is processed on-board and then downlinked over a miniaturized high-speed
Ka-band transmitter. The common satellite bus uses
reaction wheels,
magnetic torque coils,
star trackers,
magnetometers,
Sun sensors, and
gyroscopes to enable precision 3-axis pointing without the use of propellant.
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
CubeSats are smaller. Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
CubeSats are smaller. Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
CubeSats are smaller. Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).