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KazEOSat-1 satellite
KazEOSat-1 (Kazakhstan Earth Observation Satellite) is the first Kazakh satellite of remote sensing of the Earth, created by the order of Government of the Republic of Kazakhstan by the European company "Airbus Defence and Space" on the basis of satellite platform "Leostar-500-XO".
Technical characteristics of KazEOSat-1 spacecraft
Name of the spacecraft; KazEOSat-1
Country; Kazakhstan
Developer; Airbus Defence and Space
Operator; JSC Kazakstan Garysh Sapary
Launch vehicle; VEGA
Launch date; 30.04.2014
Orbit:<br>height, km<br>inclination, degree<br>circulation period, min<br>number of turns per day;Sun-synchronous<br>694<br>98.2<br>99.9<br>14.4
Platform:<br>the angles of deflection, deg;Leostar-500-XO<br>35
Period of active existence, years; 7
Size of spacecraft, m×m; 2,10х3,70
Power, W; 1200
Mass of spacecraft, kg; 820
Follow-up period, day; 3
Technical characteristics of KazEOSat-1 spacecraft shooting equipment
Name of shooting equipment;NAOMI
Diameter of the main mirror, cm; 64
Spectral ranges, microns;Panchromatic 0.45-0.75<br>Blue 0.45-0.52<br>Green 0.53-0.60<br>Red 0.62-0.69<br>Near IR 0.76-0.89
Tool weight, kg; 150
Dynamic range, bit; 12
Spatial Resolution, PAN, m; 1
MS, m; 4
Shooting bandwidth, km; 20
Data transfer rate, Mbit/sec; 270
Possibility of obtaining a stereo pair; Yes, from one turn
Capacity, sq. km/day; 220000
Main cases of using data obtained from KazEOSat-1 spacecraft: