Horizons-2 – Orbital Horizons-2 User Manual

Page 2

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Orbital Sciences Corporation

45101 Warp Drive

Dulles, Virginia 20166

www.orbital.com

©2014 Orbital Sciences Corporation

FS004_05_2998

Horizons-2

Mission Partners

Horizons Satellite Holdings, LLC

A joint venture between Intelsat and SKY Perfect JSAT

Orbital Sciences Corporation

Prime contractor for Galaxy 12, 14 and 15; Intelsat 11, 15, 16, 18,
23 and 28; and Horizons-2 for an Intelsat/SKY Perfect JSAT joint
venture

Arianespace

Launch provider

Specifications

Spacecraft

Launch Mass:

2,350 kg (5,181 lb.)

Solar Arrays:

Three panels per array, UTJ Gallium
Arsenide cells

Stabilization:

3-axis stabilized; zero momentum system

Propulsion:

Liquid bi-propellant transfer orbit system;
monopropellant (hydrazine) on-orbit system

Batteries:

Two >3850 W-Hr capacity Li-Ion batteries

Mission Life:

15 years

Orbit:

74° West Longitude

Payload

Ku-band
Repeater:

16 active transponders with 22-for-16
redundant TWTAs; 4 active transponders
with 6-for-4 redudant TWTAs

Antenna:

Two 2.3 m dual grid shaped reflectors

Launch

Launch Vehicle:

Ariane 5

Site:

Kourou, French Guiana

Date:

December 21, 2007

East Coast Coverage Area

Coverage Contour Maps

CONUS Coverage Area

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