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DOC-03 / APISAT
The system is developed as a modular payload architecture that can be integrated with a host satellite in a future mission.
| Form factor | 6U CubeSat — 10 × 20 × 30 cm |
| Primary payload | Custom optical polarimeter |
| Application | Earth observation research |
| Power system | TBD |
| Mass budget | TBD — under definition |
| Target orbit | SSO — altitude TBD |
| Communications | UHF/VHF — link budget in progress |
| Full specifications | Published at Phase 02 milestone |