KazEOSat 1 (DZZ-HR, HRES)

Kazakhstan

Spacecraft nº:

Kazakhstan spacecraft nº: 4


Launch data:

Designation 39731 / 14024A
Launch date 30 Apr 2014 - 01:38 UT
Launch site Ko, ELV
Launch vehicle  Vega (VV03)
Mission Earth observation (Imaging)
Sun-synchronous Earth orbit:
Perigee / Apogee 758 x 760 km
Eccentricity 
Inclination 98.5°
Period 99.9 min


Spacecraft data:

Prime manufacturer EADS Astrium ––> Airbus Defence and Space
Platform Leostar-500-XO
Operator Kazakhstan Gharysh Sapary (KGS)
Mass at launch  830 kg
Dry Mass  kg
Basic shape  
Dimension (m) 
Equipment 
Solar array Deployable fixed solar arrays
Stabilization  
Propulsion Hydrazine thrusters
DC power  
Design lifetime  7 yrs



Description:

Mission details:

  • Satellite tracking: Real time satellite tracking
  • Spaceflight 101: Satellite & rocket information

    Ref.: #7(JR697), #14, #110, #228 - update: 02.12.14 Home