Satellite Systems Engineering
We engineer small satellite missions end to end, from the first requirements through launch and operations.
- Mission analysis and concept design
- Requirements and interface control
- Flight and ground software
- Link, power, and mass budgets
- Orbit and coverage analysis
- Integration, test, and operations
- Orbit
- Sun-synchronous
- Altitude
- 550 km
- Inclination
- 97.6°
- Period
- 95.6 min
Digiverz