First CubeSat of Pakistan
To design, develop, test and launch a 1U pico-satellite
Mass: 1.08 Kg, Dimensions: 10cm x 10cm x10cm, Power generation: Triple junction GaAs Solar cells, Uplink : 435.060 MHz, 1200 bps AFSK, Downlink : 145.947 MHz, 1200 bps BPSK, Beacon: CW and AX25, Camera: VGA Resolution
ICUBE-1 contains two dipole antennas. One in the UHF band and the second in the VHF band. The antennas are stowed before launch and held in place using a Dyneema wire. The wire will be burned using heating elements after separation with the launch vehicle.
Test bench for the testing of ICUBE-1 IMU which includes three axis gyroscopes, three axis accelerometer, three axis magnetometer and a temperature sensor
The software decodes the received telemetry data from ICUBE-1 displaying the status of different sensors and other parameters of ICUBE-1
ICUBE-1 will be launched via Dnper-1 launch vehicle from Yasny launch base, Russia at an altitude of 600km