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: height, km inclination, degree circulation period, min number of turns per day |
Sun-synchronous 694 98.2 99.9 14.4 |
Platform: the angles of deflection, deg |
Leostar-500-XO 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 Blue 0.45-0.52 Green 0.53-0.60 Red 0.62-0.69 Near IR 0.76-0.89 |
Tool weight, kg | 150 |
Dynamic range, bit | 12 |
Spatial Resolution, PAN, m MS, m |
1 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:
- ecological monitoring;
- mapping;
- monitoring of disaster areas;
- land cadastre;
- defense and security.
For more information about the available coverage of space images from the satellite KazEOSat-1 on the territory of interest to you, send the terms of reference or the coordinates of the site by e-mail: innoter@innoter.com we will be glad to answer your questions by phone: +7 (495) 245-04-24