- Provide educational opportunity in space projects for students.
- Develop and use a Software Defined Radio and experiment full communications in-orbit reconfiguration and use.
- LEO radiation mapping using Radiation Displacement Damage Sensor (RDS), a non-ionising radiation dosimeter.
- Panel Deployment Mechanism for higher available payload power.
Mass: 0.930 kg
Perigee altitude: 300 [km]
Apogee altitude: 1500 [km]
Period: 97.49 min
Project management plan & engineering activities in collaboration with INTA.
Teams responsible for management, engineering, design and science.
Over 20 teachers, 80 students.
Launched on inaugural ESA Vega, 13th of February, 2012, Kourou ELA-1.