[Source Tsenki et RussianSpaceWeb]
MAIN CHARACTERISTICS OF THE SPACECRAFT:
Spacecraft weight, kg 1900
Scientific payload weight, kg 540
Orbit:
• type circular
• height, km 500
• inclination, deg 82.5
Accuracy of the spacecraft longitudinal axis orientation to the Sun, arc min better than 5
Determination accuracy of the spacecraft longitudinal axis orientation on the Sun, arc min 3
Angular velocity stabilization of the spacecraft, deg/s less than 0.005
Accuracy of the satellite position measurement:
• along the orbit, m ±1000
• by height and in transverse directions, m ±500
Volume of scientific information stored per day, Gbit 8.2
Information transmitted during one communication session, Mbit 2048
Nominal mission lifetime, years at least 3
Main goal of the project:
The investigation of energy accumulation and its transformation into energy of accelerated particles processes during solar flares; the study of the acceleration mechanisms, propagation and interaction of fast particles in the solar atmosphere; the study of the solar activity correlation with physical-chemical processes in the Earth upper atmosphere.