The satellite is equipped with mechanisms for deployment of solar panels to solve the classic problem of the lack of energy of this type of apparatus. The satellite provides the possibility of direct communication with the ground control centre of flight and interaction with other satellites of its own orbital constellation. It is equipped with an active orientation system to ensure the possibility of optical observation including solutions of this task within the group.
Within the framework of the creation of small space vehicles unified platforms for the construction of space vehicles with a mass of 20-80 kg are being developed. The platform is created in the format of two independent elements – a casing bearing structure and a set of on-board equipment including power supply systems, passive orientation, command radio lines, mechanisms for opening solar panels and antennas.