Official name EUTE HOT BIRD 13B (HB 8)
Alternative name Eutelsat Hotbird 13B (Hotbird 8)
Cospar ID 2006-032A
Norad ID 29270
Launch date 2006-08-04
Launch site TTMTR
Launch vehicle Proton-M Briz-M (Ph.1)
Country/Organization International
Type application Communication (Direct Broadcasting)
Operator Eutelsat
RCS size LARGE
Decay date ON ORBIT
Period (min) 1436.08
Inclination (deg) 0.05
Perigee (km) 35770
Apogee (km) 35803
Eccentricity 0.000461067721068001
Mean motion (revs. per day) 1.00272965294413
Semi-Major axis (km) 42164.635
Raan (deg) 37.991
Arg of perigee (deg) 30.5513
Shape Box + 2 Pan
Mass (kg) 4875
Height (m) 5.8
Width (m) 2.5
Depth (m) 2.5
Span (m^2) 39
Lifetime 15 years
Contractors EADS Astrium
Equipment 64 active Ku-band transponders
Propulsion ?
Configuration Eurostar-3000
Power 2 deployable solar arrays, batteries

Eutelsat and EADS ASTRIUM announced in September 2003 the signature of a contract for the construction the Hot Bird 8 broadcast satellite which was launched in early 2006 by Arianespace on-board an Ariane 5 rocket.

With 64 transponders that can be operated simultaneously, of which 58 transponders will operate at full power for most of the satellite's lifetime, Hotbird 8 is the largest satellite yet ordered by Eutelsat. It will join the company's constellation of HOT BIRD broadcasting satellites at 13° East that provide television, radio and interactive services to almost 100 million cable and satellite homes in Europe, North Africa and the Middle East.

Hotbird 8's mission is to replace existing Hotbird capacity and to join Hot Bird 7A in bringing in-orbit sparing to a level where 13° East can maintain its reputation as one of the most secure multi-satellite video neighbourhoods. The satellite has been designed to cover all 102 Ku-band transponders/frequencies at 13° East which means that it can substitute any transponder on the other Hotbird satellites.

EADS Astrium, as prime contractor for Hotbird 8, designed and built the satellite and supplied both the payload and the platform. The spacecraft will had a launch mass of less than 5 tons, a solar array span of 45 meters once deployed in orbit, and a spacecraft solar array power of almost 14 kW at end of life. It will provide commercial services for a minimum of 15 years.

Hotbird 8 is based on the Eurostar-3000 version of the Eurostar family.

An identical Hot Bird 9 was contracted in May 2006 for a launch in 2008.

In December 2011 Eutelsat announced, that their satellite assets will be renamed under a unified brand name effective from March 2012. Hot Bird 8 and 9 became Eutelsat Hot Bird 13B and 13C respectively.

The Hot Bird 10, which was ordered in October 2006 is also identical to Hot Bird 8 and Hot Bird 9 with the same mission capacity. It was initially comissioned as Atlantic Bird 4A at 7°W. When Atlantic Bird 7 became operational, it was renamed Eutelsat 3C and was colocated with Eutelsat 3A at 3° East. Later it became Hotbird 13D and in 2016 Eutelsat 33E.

Satellite COSPAR Date LS Launch Vehicle Remarks
EUTE HOT BIRD 13B (HB 8) 2006-032A 2006-08-04 TTMTR Proton-M Briz-M (Ph.1)
EUTE HOT BIRD 13C (HB 9) 2008-065A 2008-12-20 FRGUI Ariane-5ECA with Eutelsat W2M
EUTE 33E 2009-008B 2009-02-12 FRGUI Ariane-5ECA with NSS 9, SPIRALE A, SPIRALE B