The PCB is mechanically matched to the satellite structure. Its elements are selected in such a way as to ensure correct working in a wide temperature range and in unfavorable conditions prevailing in orbit. The heart of the board is the STM32 microcontroller ensuring low power consumption and high computing power.

The plate is connected to IMU sensors – an accelerometer, a magnetometer, gyroscope and a thermometer. It is thanks to the data from these sensors that we will know the current position of the satellite and find out if our experiment is successful.