Official name SUPERBIRD A1
Alternative name Superbird A1
Cospar ID 1992-084A
Norad ID 22253
Launch date 1992-12-01
Launch site FRGUI
Launch vehicle Ariane-42P H10+
Country/Organization Japan
Type application Communication
Operator Space Communications Corporation (SCC)
RCS size LARGE
Decay date ON ORBIT
Period (min) 1452.8
Inclination (deg) 11.63
Perigee (km) 36057
Apogee (km) 36168
Eccentricity 0.00153686396677051
Mean motion (revs. per day) 0.991189427312775
Semi-Major axis (km) 42490.635
Raan (deg) 27.4082
Arg of perigee (deg) 143.8114
Shape Hex Poly + 2 Pan
Mass (kg) 1650.15
Height (m) 2.4
Width (m) 2.2
Depth (m) 2.2
Span (m^2) 20.28
Lifetime 10 years
Contractors Space Systems/Loral (SS/L)
Equipment 23 Ku-band transponders, 3 Ka-band transponders, 2 X-band transponders
Propulsion R-4D-11
Configuration SSL-1300
Power 2 deployable solar arrays, batteries

Satellite news gathering, cable television distribution, video conferencing, newspaper transmission, business applications, and banking services are being delivered to Japanese customers by the two SUPERBIRD satellites built for Space Communications Corporation (SCC) of Japan by Space Systems/Loral (SS/L).

The geostationary SUPERBIRD has 23 transponders that operate in the Ku-band, at 50 and 85 Watts, three Ka-band transponders at 29 Watts, and two X-band transponders at 47 Watts. Total on-board prime dc power is 4,000 Watts.

SUPERBIRD-1 (A1) was completed in 23 months and delivered on orbit in March, 1992. SUPERBIRD-2 (B1) was completed in 19 months and delivered on orbit in February, 1993, both from the European Space Center at Kourou, French Guyana. Control after launch was provided by SS/L's Mission Control Center in Palo Alto, Calif., until completion of check-out in orbit, after which control was passed to SCC.

The SUPERBIRD spacecraft is based on SS/L's threeaxis, body-stabilized SSL-1300 bus, whose modular design has proven its worth during some 275 years of cumulative on-orbit service, close to 45% of the total of 630 plus years amassed by SS/L satellites to date.

The SSL-1300 buses achieve long useful orbital life - in this case 10 years - through use of a bipropellant propulsion system and a momentumbias system for excellent stationkeeping and orbital stability. Solar arrays and nickel-hydrogen batteries provide uninterrupted electrical power.

Satellite COSPAR Date LS Launch Vehicle Remarks
SUPERBIRD A 1989-041A 1989-06-05 FRGUI Ariane-44L H10 with DFS-Kopernikus 1
SUPERBIRD B1 1992-010A 1992-02-26 FRGUI Ariane-44L H10 with Arabsat 1C
SUPERBIRD A1 1992-084A 1992-12-01 FRGUI Ariane-42P H10+