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Apstar 7


General


Designation 38107 / 12013A
Launch date 31 Mar 2012
Country of origin China
Mission Telecommunications
Geostationary orbit 76.5°E
Launch vehicle Long March 3 #151

To replace Apstar 2R. Tested at 81.5°E

sat-index articles


Technical data


Lyngsat transponder loading


EIRP coverage (dBW)


C-band
Ku-band Africa
Ku-band China
Ku-band Middle East

Specifications


Prime contractor Thales Alenia Space
Platform Spacebus-4000C2
Mass at launch 5014 kg
Dry mass  
Dimension  
Solar array  
Stabilization 3-axis
DC power 11.4 kW
Design lifetime 15 years

C-band


Main transponders 28
Backup transponders  
Power  
Bandwidth  
Coverage Asia, Australia and part of Africa
EIRP max  
G/T max  
Polarization  

Ku-band


Main transponders 28
Backup transponders  
Power  
Bandwidth  
Coverage China
Middle-East
North Africa
African beam
Steerable beam
EIRP max  
G/T max  
Polarization  

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