The spacecraft is a three-axis, stabilised satellite, yaw/pitch/roll steering (zero Doppler), characterised by sun, star, gyro and magnetic field sensors, a set of four reaction wheels dedicated to orbit and attitude control and three torque rods as actuators to provide steering capabilities on each axis. The satellite is equipped with two solar array wings capable of producing 5 900 W (at end of life) to be stored in a modular battery, the battery capacity is 324 Ah.