Three-axis stabilized, accurate and agile attitude control for precise imaging operations.[3]
Dual redundancies are adapted where necessary in the system architecture design to increase reliability of the satellite system.[3]
Dimensions: 1.2 m in diameter and 1.35 m in height.[3]
Deck-and-longeron type structure permitting easy assembly and disassembly. The interface with the launch vehicle is made through an adapter bolted to the bottom of the structure. The mechanical interface with the electro-optical payload is provided through three points at the satellite middle deck.[3]