CESIUM MISSION 1

Cesium Mission 1 (CM1) is CesiumAstro's first mission to launch and operate our own hardware in space. CM1 provides an on-orbit platform consisting of two satellites for customer experiments that push the boundaries of small-satellite communication. In addition, it gives CesiumAstro the capability to demonstrate advanced features of our technology such as dynamic-waveform switching and dynamic-link optimization. With the launch of CM1, CesiumAstro now has a complete commercial phased array communication system as well as an intersatellite link in LEO.

The CM1 ground segment includes CesiumAstro ground stations and the GlobalStar network for persistent command and telemetry. CesiumAstro is developing ground stations at office locations in Texas and Colorado. These ground stations can communicate with the spacecraft over both payload and telemetry links.  Additionally, the ground stations are remote-operable on the CesiumAstro network across CesiumAstro locations.

ON-ORBIT 
EXPERIMENT PLATFORM

CS1 and CS2 PAYLOAD

Cesium Satellites 1 and 2 are 6U cube-sats with CesiumAstro Nightingale I active phased array and intersatellite link payloads. The spacecrafts have a high-accuracy attitude system with a star tracker and state-of-the-art electric propulsion system.

satellite mission moon

CM1 CONOPS

LAUNCH

Cesium Satellite 1 and 2 launched to orbit in 2021 on the Atlas V-401 Rocket.

PAYLOAD DELIVERY

Rocket upper stage reaches primary payload orbit (2) and primary payload is deployed (3). Rocket upper stage transfers to 550km orbit (4) and Cesium Satellite 1 and 2 are deployed (5).

MANEUVER 1

Low-thrust inclination change from 97.6° Sun-synchronous orbit to non-Sun-synchronous orbit.

ORBIT ROTATION

Orbit rotation to dawn-dusk orbit.

MANEUVER 2

Low-thrust inclination change to Sun-synchronous orbit for operations at dawn-dusk 550km.

DECOMMISSION

Decommissioning phase, low-thrust spiral to deorbit.