This CubeSat is equipped with advanced sensors, high-resolution cameras, and communication systems that enable it to perform tasks such as Earth observation, atmospheric studies, and space weather monitoring. Its compact design and efficient power management make it an ideal platform for educational institutions and research organizations looking to conduct space-based experiments.
memory Mission Specs
Launch Mass
6.5 kg
Dimensions
60x20x20 cm
Design Life
1 year
Orbit
LEO
Download Resources
Research Opportunities
Apply for payload time on the Orion 2 mission.
view_in_ar Interactive 3D Model
Explore the Orion 2 structure with deployed solar arrays. Drag to rotate, scroll to zoom.
Assembly Process Gallery
Chassis Integration
Solar Panel Test
Thermal Vacuum
Mission Lifecycle & Goals
architecture
Concept & Design
Defining scientific objectives and payload requirements for Low Earth Orbit (LEO) experiments. The modular architecture is finalized to support diverse sensor arrays.