Thaicom-3

Overview :
THAICOM-3 was a three-axis stabilized spacecraft with a payload capacity of 25 C-Band and 14 Ku-Band transponders. After nine years in operation and relocated to its new position at 50.5 degrees East, THAICOM 3 satellite was deorbited after experiencing power loss to such an extent that it could not provide further service on October 2, 2006.
Footprint Map :
Specifications :

Footprint Map :
A
C-Band Global Beam B
C-Band Regional Beam C
Ku-Band Spot Beam D
Ku-Band Steerable Beam
Specifications :
Design |
: |
Aerospatiale SpaceBus 3000A |
Power System |
: |
5300 Watts |
Launch Weight |
: |
2652 Kg. |
Mass in Orbit |
: |
1560 Kg. At the beginning of spacecraft's life |
End of Life |
: |
9 years (Deorbited on Oct 2,2006) |
Transponder Capacity |
: |
C-Band = 7 (Global) + 6 (Regional)=13 (each 36 MHz) |
Satellite Location |
: |
78.5 degrees East |
Launch Agency |
: |
Arianespace of France. |
Launch Date |
: |
April 16, 1997 |
Service Date |
: |
May 1997 |