CubeSat Class | 8 kg |
CubeSat Size (Stowed) | 22 x 10 x 36 (6U) 22 x 10 x 45 cm (6U XL) |
Bus Architecture | Failure-tolerant |
Available Payload Mass | ~4 kg |
Available Payload Volume | 2U – 5U |
Average Payload Power Available | 10 W (Si cells), 20 W (GaAs cells) peak per channel 20 / 30 W (up to five channels) bus voltage: 12 V nominal |
Attitude control | Determination < ± 1 ° (MEMS sun sensor, magnetometer, gyro) Pointing < ± 5 ° (3-axis by reaction wheels, magnetorquer) |
Telemetry and Telecommand | 2.0/2.2 GHz (S-band, FDD) upto 100 kbps (Uplink) upto 2 Mbps (Downlink) |
Data Link | 8 GHz (X-band) upto 100 Mbps |
Orbit | < 650 km (20 years orbit time according to European code of conduct for space debris mitigation) |
Design lifetime | 2 years |