Explore this platform:
Why HyperSat Nano?
The smallest HyperSat platform: a 1/4-plate nano/microsatellite for missions where unit cost, future development needs for larger satellite platform, time to orbit and constellation scalability are decisive. Adaptable for Earth Observation, Space Situational Awareness, RF signal collection and In-Orbit Demonstration. Flight-proven since 2025.Selected Technical Specifications:Mass, Size & Power: ~ 60 kg satellite wet mass, SpaceX 1/4 plate mini/nanosatellite; OAP up to 65W.Heritage: first flight: Gen 1.0 - Q4 2025 (PIAST mission, Gen 2.0 planned for Q4 2027; in total 3 satellites based on Nano platform already delivered and one more on order.Propulsion: available, allows altitude changes up to 100 km, station keeping & debris avoidance.Agility: 1 deg/s slew rate.
Explore product
Payload bay:
up to 15 kg of integrated instruments in a 1/4 plate satellite
Constellation economics:
non-redundant avionics and a standardised build reduce unit cost and lead time, allowing coverage to be built from several units rather than one.
Exemplary use cases:
Moderate-Resolution (MR) visible (VIS+) Earth Observation, Internet of Things, space weather and debris monitoring, in-orbit tests and experiments.
What you get:
A cost-effective, ITAR-free nano/microsatellite platform and a set of additional, on-demand services:
End-to-end mission management, a full coverage from design review to end of life
Ground Segment as a Service, shared antenna network and mission control, with no ground infrastructure capex on your side
Launch campaign support - launcher selection, integration, licensing and shipment
Training and knowledge transfer - sovereign capabilities built in-house
Cooperation scenarios tailored to your needs:
Discover HyperSat Nano
Turnkey satellite with preintegrated payload (see satellites section)
Customer payload integration
Payload selection based on Client End User requirements
Launcher compatibility:
Multiple launchers available
Technical Specification
AttributeCommunication
Standards implemented: CCSDS, PUS-C
Encryption: AES-128, SDLS-compliant
Uplink: S-band, 128 kbps
Downlink: S-band up to 1Mbps / X-band up to 500 Mbps
Payload Interfaces and Data Storage:
Telemetry and Telecommand (TM/TC) interfaces:
Daily imaging rate: 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
