ION Satellite
Bus Specs
ION Satellite
Bus Specs
D-Orbit ION
D-Orbit ION
Lifetime
Lifetime
5 Years
5 Years
Altitude
Altitude
450-750 km without propulsion, 2000 km with propulsion
450-750 km without propulsion, 2000 km with propulsion
Power (panel)
Power (panel)
497 W (BoL), 392 W (EoL)
497 W (BoL), 392 W (EoL)
Power (OAP)
Power (OAP)
226 W Spacecraft OAP
226 W Spacecraft OAP
Battery
Battery
570 Wh (BoL), 428 Wh (EoL)
570 Wh (BoL), 428 Wh (EoL)
Bus Voltage
Bus Voltage
50V, with 32V regulated output for payload
50V, with 32V regulated output for payload
Payload Mass (kg)
Payload Mass (kg)
200 kg
200 kg
T&C
T&C
Omnidirectional S-Band: 500 kbps
Omnidirectional S-Band: 500 kbps
Payload Downlink
Payload Downlink
Directional X-Band: 50 Mbps (current), 400 Mbps (future)
Directional X-Band: 50 Mbps (current), 400 Mbps (future)
ISL
ISL
Contact us for optical or RF options
Contact us for optical or RF options
Pointing Accuracy
Pointing Accuracy
< 1 deg (3 sigma)
< 1 deg (3 sigma)
Pointing Stability
Pointing Stability
D-Orbit system incorporates a payload deck, which is mechanically isolated from the reaction wheel cluster, reducing total jitter from vibration < 0.005 arcSec
D-Orbit system incorporates a payload deck, which is mechanically isolated from the reaction wheel cluster, reducing total jitter from vibration < 0.005 arcSec
Propulsion
Propulsion
Contact us for EP or chemical propulsion options
Contact us for EP or chemical propulsion options
© 2024 D-Orbit USA ALL RIGHTS RESERVED
© 2024 D-Orbit USA ALL RIGHTS RESERVED
© 2024 D-Orbit USA ALL RIGHTS RESERVED