The CubeADCS from CubeSpace is a low-power Attitude Determination and Control System (ADCS) that is designed for use in nanosatellites with a form factor of 2 to 16 U and can be configured for use in large satellites. It has a mass of less than 0.3 Kg. It consists of an ADCS computer with a 3-axis MEMS rate sensor, a deployable magnetometer, coarse sun sensors, a redundant magnetometer, fine sun & earth sensors, and a star tracker. This ADCS system has three default modes that can provide detumbling of the satellite, attitude stabilization in the orbit, and perform pitch maneuvers. This system measures 90 x 96 x 48 mm.