Official name ANIK F3
Alternative name Anik F3
Cospar ID 2007-009A
Norad ID 31102
Launch date 2007-04-09
Launch site TTMTR
Launch vehicle Proton-M Briz-M (Ph.1)
Country/Organization Canada
Type application Communication
Operator Telesat Canada
RCS size LARGE
Decay date ON ORBIT
Period (min) 1436.12
Inclination (deg) 0.01
Perigee (km) 35778
Apogee (km) 35796
Eccentricity 0.000251487970492078
Mean motion (revs. per day) 1.00270172408991
Semi-Major axis (km) 42165.135
Raan (deg) 308.5149
Arg of perigee (deg) 91.357
Shape Box + 2 Pan
Mass (kg) 4640
Height (m) 4.8
Width (m) 2.4
Depth (m) 2.4
Span (m^2) 35
Lifetime 15 years
Contractors Astrium
Equipment 24 C-band transponders, 32 Ku-band transponders, 2 Ka-band transponders
Propulsion ?
Configuration Eurostar-3000S
Power 2 deployable solar arrays, batteries

EADS Astrium has been selected by Telesat to build the company's new Anik F3 satellite. Planned to enter into service in 2006, Anik F3 will provide satellite communications services in C, Ku and Ka-bands over a large area covering North America from its orbital location of 118.7º West.

EADS Astrium, as prime contractor for Anik F3, will design and build the satellite and supply both the payload and the platform. Canadian industry will supply a significant part of the spacecraft equipment and technology. The satellite will provide a full range of satellite communications services that include telephony, business communications, Internet-based services and television transmission and is equipped with 24 active transponders in C-band, 32 in Ku-band and 2 in Ka-band.

The spacecraft will have a launch mass of 4.6 tons, a solar array span of 35 meters once deployed in orbit, and spacecraft power of 10 kW at end of life. The satellite, operating in geostationary orbit, will provide commercial services for a minimum of 15 years.

Satellite COSPAR Date LS Launch Vehicle Remarks
ANIK F3 2007-009A 2007-04-09 TTMTR Proton-M Briz-M (Ph.1)