Technical Specifications

• Orbit: GEO Orbit
• Mass: ~1000 kg - 3000 kg
• Power Capacity: ~7.5 kW (end of life)
• Design Life Time: >15 years
• Compatible Launchers for Multi-Launch: Ariane VI, FALCON 9, Blue Origin, PROTON, Soyuz
• Strategic Advantages:
  • Cost-effective system solution with multiple launch configuration
  • Electric propulsion system
  • Software-based flexible communication payload
  • Digital beamforming and beam steering
  • Short lead time