Ses-8 – Orbital SES-8 User Manual
Page 2

Orbital Sciences Corporation
45101 Warp Drive
•
Dulles, Virginia 20166
•
www.orbital.com
©2014 Orbital Sciences Corporation
FS003_11_2998
Coverage Contour Maps
Indo-China EIRP 95
°
East Longitude
SES-8
Specifications
Spacecraft
Launch Mass:
3,200 kg (7,055 lb.)
Solar Arrays:
Four panels per array, UTJ Gallium
Arsenide cells
Stabilization:
3-axis stabilized
Propulsion:
Monopropellant (hydrazine) on-orbit system
Batteries:
Two >4840 W-Hr capacity Li-Ion batteries
Mission Life:
15 years
Orbit: 95
°
East Longitude
Payload
Ku-band
Repeater:
24 active transponders with one group of 18-
for-15; one group of 12-for-9 TWTAs
TWTA Power:
120 W RF
Antenna:
Two 2.5 x 2.7 m single shell super-elliptical
deployable reflectors; one 1.45 m single shell
deck-mounted
Launch
Launch Vehicle:
Falcon 9
Site:
Cape Canaveral, Florida
Date:
December 3, 2013
Mission Partners
SES
A leading global satellite operator providing a broad range of
communications services
Orbital Sciences Corporation
Prime contractor for the SES program
South Asia EIRP 95
°
East Longitude
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