Kazeosat-1

Spacecraft propulsion supplied by ArianeGroup

Kazeosat-1
	Category	Earth Observation
	Operator	Kazakhstan Gharysh Sapary
	Orbit	LEO
	Sat position	738 × 742 km
	Launch date	30.04.2014
	Launch mass	830 kg
	Design life	7.25 years
	Launcher	Vega
	Satellite / Bus	Leostar 500-XO
	Manufacturer	EADS Astrium

Orbital Propulsion Centre Contribution
Propulsion Responsibility: Complete system, incl: 4 x 1 N hydrazine thrusters Pyrovalve Latch valve 3 x Fill & drain valves