Garuda 1
Launch cost: $70 million.
The operator successfully clained $101.5 million from insurance for the anomaly
on the L-band system which reduces the maximum calling capacity (1.4 million a
day instead of 2 million planned).
Went inclined in Jun 2005.
Out
of service
|
Jan
2015
|
Cause
|
moved
to Junk orbit
|
sat-index articles
Prime
contractor
|
Lockheed
Martin
|
Platform
|
A2100AXX
|
Mass
at launch
|
4400
kg
|
Mass
in orbit
|
|
Dimension
|
|
Solar
array
|
|
Stabilization
|
3-axis
|
DC
power
|
BOL:
14000 W
EOL: 9000 W
|
Design
lifetime
|
12
years
|
Main
transponders
|
88
|
Backup
transponders
|
22
|
Power
|
SSPAs
|
Bandwidth
|
|
Coverage
|
22
countries: from Guam to Papua New Guinea in the east to Pakistan in the west,
and from Japan in the north to Indonesia in the south
12 beams
|
EIRP
max
|
73
dBW
|
G/T
max
|
15.3
dB/K
|
Polarization
|
|
2 antennas each 12 m diameter (to be built by Harris Aerospace (US))
Main
transponders
|
|
Backup
transponders
|
|
Power
|
|
Bandwidth
|
|
Coverage
|
|
EIRP
max
|
|
G/T
max
|
|
Polarization
|
|