|Operator||Intelsat/SKY Perfect JSAT Group|
|Mission duration||15 years|
|Launch mass||2,350 kilograms (5,180 lb)|
|Start of mission|
|Launch date||21 December 2007, 21:41:55UTC|
|Launch site||Kourou ELA-3|
|Longitude||74° west (2008-2011)|
84.9° east (2011—)
|Coverage area||Continental United States|
|EIRP||3.5 kilowatts (minimum EOL)|
Platform and payload
Horizons-2 was built by Orbital Sciences Corporation based on its STAR-2 satellite platform, which will generate 3.5 kilowatts of payload power by means of two solar arrays, each equipped with three panels of UJT gallium arsenide cells. The solar arrays charge two lithium ion batteries with capacities of at least 3,850 watt-hours.
The spacecraft is 3-axis stabilized, with a zero momentum system. Hydrazine-fuelled monopropellant thrusters are used for stationkeeping, with an IHI BT-4 bipropellant engine used for insertion into geostationary orbit. It has a design life of 15 years; however, it is fuelled for at least 16 years of operations. Its payload consists of 20 Ku-band transponders broadcasting through two 2.3-meter (7.5 ft) dual gridded shaped reflectors.
 It has 16 active transponders with 22-for-16 redundant 85 W TWTAs and four active transponders with 6-for-4 redundant 150 W TWTAs. The satellite will provide service to the continental United States, the Caribbean and parts of Canada.
- "Arianespace to launch two Intelsat payloads". Arianespace. Archived from the original on 2007-06-13.
- "Sixth successful Arianespace mission in 2007: RASCOM-QAF1 and Horizons-2 in orbit". Arianespace. Archived from the original on 2015-10-31.
- "Orbital ATK" (PDF). Orbital.com. Retrieved 9 August 2017.