AS9100 and ISO 9001 Registered  
Satellites & Space
Systems
Space Launch
Vehicles
Missile Defense
Systems
Human Spaceflight &
Exploration Systems
Space Technical
Services
Communications Satellites
Thaicom 6
SES-8
MEXSAT-3
Azerspace
Star One C3
HYLAS 2
Intelsat 23
Intelsat New Dawn
Intelsat 18
KOREASAT 6
SES-1, -2 & -3
Intelsat 15
Intelsat 16
NSS-9
MEASAT-3a
AMC-21
THOR 5
Horizons-2
Intelsat 11
Optus D1, D2 & D3
TELKOM-2
Galaxy 12, 14 & 15
N-STAR c
BSAT
IndoStar-1
ORBCOMM
Science & Technology Satellites
Imaging & Defense Satellites
Hosted Payloads
Ground Systems & Customer Support
Orbital’s STAR Geosynchronous
Satellites brochure (PDF)
Orbital's STAR brochure
The compatibility of our STAR GEO platform with a variety of launch vehicles
The compatibility of our STAR GEO platform with a variety of launch vehicles
Information about our GEO satellite customer support
Information about our GEO satellite customer support
Details of our 125,000 sq. ft. Satellite Manufacturing Facility
Details of our 125,000 sq. ft. Satellite Manufacturing Facility
STAR Bus Hosted Payloads
STAR™ Bus Hosted Payloads
Intelsat 23

Intelsat-23

Orbital is building the Intelsat-23 (IS-23) GEO communications satellite for Intelsat, LLC.  IS-23 will generate 4.8 kilowatts of electrical payload power and carry 15 active Ku-band and 24 active C-Band transponders.  The spacecraft will provide communications services for the Americas, Caribbean, Western Europe, Africa and selected islands of the Pacific and Atlantic oceans.  Designed for a useful life of at least 15 years, the IS-23 satellite will be located in orbit at 307 degrees East Longitude following its launch in late 2011.  The IS-23 is the 10th Orbital-built geosynchronous communications satellite in the Intelsat fleet.

Performance:

C-band
Repeater: 24 active transponders with two groups of 16-for-12 redundant TWTAs
Antenna: 2.5 x 2.7 m single shell super-elliptical deployable reflector; 1.3 x 1.65 m single shell super-elliptical deck-mounted antenna

Ku-band
Repeater: 15 active transponders with 19-for-15 TWTAs
Antenna: 2.5 x 2.7 m single shell super-elliptical deployable reflector

Stabilization: 3-axis stabilized; zero momentum system
Launch Mass: 3,200 kg (7,055 lb.)
Mission Life: 15 years (fueled for 16 years)

Status:
In development.

Coverage:
The Americas, Caribbean, Western Europe, Africa and selected islands of the Pacific and Atlantic oceans

The Americas, Caribbean, Western Europe, Africa and selected islands of the Pacific and Atlantic oceans

Customer:
Intelsat - Luxembourg

Mission:
C- and Ku-Band Communications

Corporate Information | Investor Relations | News Room | Images/Video | Careers | Suppliers | Company Store | Contact

Facebook Follow us on Twitter! YouTube Flickr

©2012 Orbital Sciences Corporation. All Rights Reserved