Gsat 19e
Experimental satellite to test a new bus, and new thermal radiators, electrical
propulsion and new batteries
To provide IP services
Begin
|
End
|
Position
|
L:
|
Dec
2017
|
82.5°E
|
Feb
2018
|
|
48°E
|
sat-index articles
Lyngsat
transponder loading
Prime
contractor
|
ISRO
|
Platform
|
I-6000
|
Mass
at launch
|
3136
kg
|
Dry
mass
|
|
Dimension
|
|
Solar
array
|
|
Stabilization
|
electric
propulsion
|
DC
power
|
5.6
kW
|
Design
lifetime
|
10
years
|
Also carries spectrometer (GRASP) to study the GEO environment.
Main
transponders
|
|
Backup
transponders
|
|
Power
|
|
Bandwidth
|
|
Coverage
|
|
EIRP
max
|
|
G/T
max
|
|
Polarization
|
|
Main
transponders
|
|
Backup
transponders
|
|
Power
|
|
Bandwidth
|
|
Coverage
|
|
EIRP
max
|
|
Polarization
|
|
Frequencies
|
Uplink:
Downlink:
|