Orbit KOMPSAT-2 operates in a near-polar, circular
Sun-synchronous orbit. The orbital parameters are: • Mean altitude: 685 km • Mass: 800 kg • Inclination: 98.1° (Sun-synchronous orbit) • Orbital period: 98.6 minutes • Orbital cycle: 28 days
Instruments KOMPSAT-2's instruments are designed to acquire high- and very-high-resolution imagery with a footprint of 15 km. The satellite has the capacity to acquire 20 minutes of imagery on each orbit and it can steer its sensors both ways out to 30° off track. Panchromatic and multispectral images can be acquired at the same time. KOMPSAT-2 radiometer features:
Ground receiving stations Two receiving stations deliver KOMPSAT-2 imagery 1 to 3 days after acquisition and in under 24 hours in Europe. The
Deajeon station in
South Korea is responsible for tasking the satellite. The
Toulouse station in France is responsible for updating the catalogue, producing imagery and delivering it to its customers. == Advantages and applications of KOMPSAT-2 imagery ==