- 3U Satellite developed in collaboration with the University of Brasilia.
- Formed of two redundant sectors, A and B. The Aerospace Technologies Group developed the B sector of the satellite.
- Including a UHF Machine to Machine (M2M) payload compatible with the HumSAT protocol.
Mass: 4 kg
Perigee altitude: 396 km
Apogee altitude: 408 km
Launched from the International Space Station in 2016.
Operated successfully during 6 months before natural re-entry.