Official name GALAXY 26 (TELSTAR 6)
Alternative name Galaxy 26 (Intelsat Americas 6, IA 6, Telstar 6)
Cospar ID 1999-005A
Norad ID 25626
Launch date 1999-02-15
Launch site TTMTR
Launch vehicle Proton-K Blok-DM3
Country/Organization USA
Type application Communication
Operator Loral Skynet → Intelsat
RCS size LARGE
Decay date ON ORBIT
Period (min) 1454.62
Inclination (deg) 10.06
Perigee (km) 36128
Apogee (km) 36169
Eccentricity 0.000567105135759437
Mean motion (revs. per day) 0.989949265100164
Semi-Major axis (km) 42526.635
Raan (deg) 53.706
Arg of perigee (deg) 67.5897
Shape Box + 1 Pan
Mass (kg) 3670
Height (m) 5.3
Width (m) 2.4
Depth (m) 2.4
Span (m^2) 31
Lifetime 12 years
Contractors Space Systems/Loral (SS/L)
Equipment 24 C-band, 28 Ku-band transponders (#5, 6); 24 C-band, 24 Ku-band transponders (#7)
Propulsion R-4D-11
Configuration SSL-1300
Power 2 deployable solar arrays, batteries

Under a contract with Loral Skynet Satellite Services, Space Systems/Loral (SS/L) has built and launched three new-generation communications satellites, Telstar 5,6 and 7. Launched in 1997, Telstar 5, is the highest capacity satellite in the U.S. telecommunications industry.

The three spacecraft will serve the United States, southern Canada, Mexico, and the Caribbean. Since the satellites are delivered in orbit, SS/L assumes complete responsibility for launch services and risk management.

The hybrid Telstar 5 and Telstar 6 are each outfitted with 24 C-band and 28 Ku-band transponders and generate a total of 3200 watts of on-board transmitter power.  Telstar 7 carries 24 C-band and 24 Ku-band transponders but use more powerful components to provide identical rf power.

Lightweight composite materials and highly efficient techniques for dissipating thermal energy and for generating and storing electricity allow for a substantial increase in the spacecraft abilities, with almost no increase in size and weight.

The three geostationary Telstar spacecraft are based on SS/L's three-axis, body-stabilized 1300 platform. SS/L's 1300 buses are designed to achieve long useful orbital life - in this case 12 years - through use of a bipropellant propulsion system and a momentum-bias system for excellent stationkeeping and orbital stability. Solar arrays and nickel-hydrogen batteries provide uninterrupted electrical power.

Loral anounced in July 2003 a definite agreement to sell Telstar 5, 6 and 7 to Intelsat, who operated the satellites now as Intelsat Americas 5, 6 and 7. Intelsat changed the name of the Intelsat Americas satellites to Galaxy 25, 26 and 27 effective to 1 February 2007.

Telstar 6 suffered a control processor failure in 2001, but no service loss occured. Intelsat Americas 7's electrical-distribution system suddenly failed on 28 November 2004. Contact was regained a few days later, with 22 transponders returning to operation.

Galaxy 26 reached its operational end of life on 7 June 2014, when the final command was sent.

Galaxy 27 was retired in 2016 and was moved into a graveyard orbit above the geostationary belt.

Satellite COSPAR Date LS Launch Vehicle Remarks
GALAXY 25 (TELSTAR 5) 1997-026A 1997-05-24 TTMTR Proton-K Blok-DM4
GALAXY 26 (TELSTAR 6) 1999-005A 1999-02-15 TTMTR Proton-K Blok-DM3
GALAXY 27 (TELSTAR 7) 1999-052A 1999-09-25 FRGUI Ariane-44LP H10-3