Heritage:
Gen 1.0 first flight planned for 2029
Heritage:
Gen 1.0 first flight planned for 2029
Propulsion:
Available, allows altitude changes up to 100 km, station keeping & debris avoidance. Baseline deltaV: 280 m/s
Agility:
1 deg/s slew rate
Mass, Size & Power:
Up to 300 kg satellite wet mass, SpaceX full plate minisatellite


Turnkey satellite with preintegrated payload (see satellites section)
Customer payload integration
Payload selection based on Client End User requirements
Multiple launchers available
Standards implemented: CCSDS, PUS-C, optional incorporation of Optical Intersatellite Link (OISL)
Encryption: AES-256, SDLS-compliant
Uplink: S-band, 128 kbps
Downlink: S-band up to 1Mbps / X-band up to 500 Mbps
Telemetry and Telecommand (TM/TC) interfaces: RS-485, CAN, SpaceWire, LVDS
Data interfaces: Ethernet, 1000BASE-T
Timing interfaces: PPS, LVDS/RS-422
Data storage: min. 256GB (with payload adapter), max 2TB