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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".

Almaty, Kazakhstan, from satellite images of KA KazEOSat-1 © JSC Kazakhstan Garysh Sapary
Almaty, Kazakhstan, from satellite images of KA KazEOSat-1 © JSC Kazakhstan Garysh Sapary
Pyongyang, North Korea, satellite image KazEOSat-1 © JSC Kazakstan Garysh Sapary, resolution 1 m
Pyongyang, North Korea, satellite image KazEOSat-1 © JSC Kazakstan Garysh Sapary, resolution 1 m
Huelva, Spain, satellite image KazEOSat-1 © JSC Kazakstan Garysh Sapary
Huelva, Spain, satellite image KazEOSat-1 © JSC Kazakstan Garysh Sapary
Moscow, satellite image KazEOSat-1 © JSC Kazakstan Garysh Sapary, shooting date 15.09.2014
Moscow, satellite image KazEOSat-1 © JSC Kazakstan Garysh Sapary, shooting date 15.09.2014
Moscow, VDNKH, satellite image KazEOSat - 1 © JSC Kazakstan Garysh Sapary, shooting date 15.09.2014
Moscow, VDNKH, satellite image KazEOSat - 1 © JSC Kazakstan Garysh Sapary, shooting date 15.09.2014
Construction of the Dmitrov highway and MKAD interchange, photo from kazeosat-1 © Kazakstan Garysh Sapary JSC, 15.09.2014
Construction of the Dmitrov highway and MKAD interchange, photo from kazeosat-1 © Kazakstan Garysh Sapary JSC, 15.09.2014

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


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