Triton-X, our next generation multi-mission microsatellite designed to enable affordable regional and global LEO constellations

Earth Observation |
|
Sat mass / volume | 65kg / 40x50x60cm³ |
Payload | 30W (OAP) / 15kg for high resolution camera allowing GSD[PAN] <2m @ 550km and 16km swath |
Data | S/C/X/Ka downlink via two ground stations |
Orbit | LEO; Control optional: Chemical or electrical propulsion (delta v: ~300m/s) |
Communications |
|
Sat mass / volume | 80kg / 40x50x90cm³ |
Payload | 70W (OAP) / 30kg for IoT, M2M with scalable patch antenna array depending on coverage requirement (regional, global); |
Data | UHF/VHF/S/C/L/X/Ka-band with global ground station network and/or ISL |
Orbit | LEO; Control: Electric propulsion (delta v: 300 – 900m/s) depending on deployment and maintenance strategy |
Situational Awareness |
|
Sat mass / volume | 80kg / 40x50x90cm³ |
Payload | 70W (OAP) / 30kg OAP for Signal intelligence, Radar, GNSS reflectometry, AIS, ADS-B, VDES |
Data | UHF/VHF/S/C/X/Ka-band with global ground station network and/or Intersatellite link (ISL) |
Orbit | LEO; Control: Electric propulsion (delta v: 300 – 900m/s) depending on deployment and maintenance strategy |
Technology demo |
|
Sat mass / volume | 75 kg / 40x50x90cm³ |
Payload | 50W (OAP) / 20 kg Versatile standardised payload suite |
Data | C/X/Ka Downlink via two ground stations |
Orbit | LEO and beyond; Control: Electric propulsion (delta v: 300 – 1000m/s) depending on deployment and maintenance strategy |
Earth Observation
Sat mass / volume
65kg / 40x50x60cm³
Payload
30W (OAP) / 15kg for high resolution camera allowing GSD[PAN] <2m @ 550km and 16km swath
Data
S/C/X/Ka downlink via two ground stations
Orbit
LEO; Control optional: Chemical or electrical propulsion (delta v: ~300m/s)
Communications
Sat mass / volume
80kg / 40x50x90cm³
Payload
70W (OAP) / 30 kg for IoT, M2M with scalable patch antenna array depending on coverage requirement (regional, global)
Data
UHF/VHF/S/C/L/X/Ka-band with global ground station network and/or ISL
Orbit
LEO; Control: Electric propulsion (delta v: 300 – 900m/s) depending on deployment and maintenance strategy
Situational Awareness
Sat mass / volume
80kg / 40x50x90cm³
Payload
70W (OAP) / 30kg OAP for Signal intelligence, Radar, GNSS reflectometry, AIS, ADS-B, VDES
Data
UHF/VHF/S/C/X/Ka-band with global ground station network and/or Intersatellite link (ISL)
Orbit
LEO; Control: Electric propulsion (delta v: 300 – 900m/s) depending on deployment and maintenance strategy
Technology Demo
Sat mass / volume
75kg / 40x50x90cm³
Payload
50W (OAP) / 20kg Versatile standardised payload suite
Data
C/X/Ka Downlink via two ground stations
Orbit
LEO and beyond; Control: Electric propulsion (delta v: 300 – 1000m/s) depending on deployment and maintenance strategy