Heritage:
First flight: version 1.0 – Q3 2024 (EagleEye Mission). Version 2.0, in orbit since Q2 2026.
A fully redundant ESPA-class microsatellite platform with the most flight heritage in the HyperSat family -designed for multi-year missions and demanding instruments.Adaptable for Earth Observation, science, Space Situational Awareness/Space Surveillance and Tracking and custom missions. First flight Q3 2024, Gen 2.0 flight-proven in 2026.Why HyperSat Eagle?Large payload bay: up to 30 kg of integrated instruments in an ESPA-class, 1/2 plate satellite.Multi-year missions: full avionics redundancy so that a single subsystem failure does not end or interrupt the mission, supporting continuous space operations for up to 5 years.Exemplary use cases: High-Resolution (HR), Visible andNear-Infrared (VNIR) Earth Observation, Mid-Resolution (MR) Thermal Infrared (TIR) Earth Observation, RF signal collection, space infrastructure and debris monitoring.
Explore product
Propulsion:
Available, allows altitude changes up to 100 km, station keeping & debris avoidance. Baseline deltaV: 280 m/s
Agility:
High agility - allows dynamic capture of multiple images alternating between -30 deg and + 30 deg roll angle.
Typical latency over Europe:
~90 minutes (ground-station dependent)
What you get:
A versatile, ITAR-free small satellite 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 Eagle Platform
Turnkey satellite with preintegrated payload (see satellites section)
Customer payload integration
Payload selection based on Client End User requirements
Launcher compatibility:
Multiple launchers available
Mass, Size & Power:
120-160 kg satellite wet mass, SpaceX ½ plate minisatellite
OAP up to 110 W
Technical Specification
AttributeCommunication
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
Payload Interfaces and Data Storage:
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
