TurkmenÂlem 52E/MonacoSat

Turkmenistan, Monaco

Spacecraft nº:

Turkmenistan spacecraft nº: 2


Launch data:

Designation 40617 / 15023A
Launch date 27 Apr 2015 - 23:03 UT
Launch site CC, SLC-40
Launch vehicle  Falcon-9 v1.1
Mission Communication
Geostationary orbit:
Perigee / Apogee 35784 x 35788 km
Eccentricity 
Inclination  0.1°
Period  min
Turkmenalem 52E



Spacecraft data:

Prime manufacturer Thales Alenia Space (Cannes, FR)
Platform Spacebus-4000C2
Operator Turkmen Ministry of Communications; Space Systems International-Monaco S.A.M.
Mass at launch  4700 kg
Dry Mass  kg
Basic shape  
Dimension (m) 
Equipment 38 active Ku-band transponders
Solar array 2 deployable solar arrays
Stabilization  
Propulsion S400
DC power  
Design lifetime  16 yrs

Location:

DatePositionRemarks
 May 2015  52.0° E 



Description:

Mission details:


Ref.: #7(JR712), #14 - update: 31.07.15 Home