Official name ANIK B1 (TELESAT-4)
Alternative name Anik B1
Cospar ID 1978-116A
Norad ID 11153
Launch date 1978-12-16
Launch site AFETR
Launch vehicle Delta-3914
Country/Organization Canada
Type application Communication
Operator Telesat Canada
RCS size LARGE
Decay date ON ORBIT
Period (min) 1442.79
Inclination (deg) 10.88
Perigee (km) 35847
Apogee (km) 35988
Eccentricity 0.00196283148882857
Mean motion (revs. per day) 0.998066246647121
Semi-Major axis (km) 42295.635
Raan (deg) 321.351
Arg of perigee (deg) 313.4066
Shape Hex Poly + 2 Pan
Mass (kg) 469.77
Height (m) 3.28
Width (m) 2.05
Depth (m) 3.28
Span (m^2) 3.28
Contractors RCA Astro
Equipment 12 C-band transponders, 6 Ku-band transponders
Propulsion SVM-7
Configuration AS-3000
Power 2 deployable solar arrays, batteries

Because of the success of the Hermes program and under an arrangement between Telesat Canada and the federal government, the next satellite commissioned by Telesat - Anik B - was equipped with 4 experimental 14/12 GHz transponders in addition to 12 commercial radio frequency channels in the 6/4 GHz band used by the earlier Anik A satellites. Spacecraft construction was awarded to RCA Astro-Electronics Division.

The launch of Anik-B, on 5 December 1978 ushered in the first commercial Direct Broadcast Satellite Service (DBS). It was also the first hybrid satellite having channels in both the 6/4 GHz band and in the 14/12 GHz band. It was both a commercial satellite and an experimental platform for the Government of Canada. The former Department of Communications (DOC), in particular the Communications Research Centre (CRC) leased all of the four 14/12 GHz transponders for a two-year period, to carry on work started with the Hermes/CTS satellite. The 6/4 GHz system was used by Telesat to replace the operational capacity provided by one of the Anik-A series satellites.

Anik-B used a 3-axis stabilized spacecraft which was station-kept to within ±0.05° North-South and East-West. As a result, ground station antennas did not need to track the satellite. In the 14/12 GHz portion of the spacecraft, there were four 20W TWTAs which feed four spot beams. Two TWTAs were used for two western beams and two were used for two eastern beams, for all Canada coverage.

The EIRP of 51 dBw maximum was considerably less than that of Hermes but was typical of the power levels of commercial satellites that operated in the fixed service.

Satellite COSPAR Date LS Launch Vehicle Remarks
ANIK B1 (TELESAT-4) 1978-116A 1978-12-16 AFETR Delta-3914 with DRIMS