Official name STTW-5
Alternative name STTW-5
Cospar ID 1991-088A
Norad ID 21833
Launch date 1991-12-28
Launch site XSC
Launch vehicle CZ-3
Country/Organization China
Type application Communication
RCS size LARGE
Decay date ON ORBIT
Period (min) 632.57
Inclination (deg) 31.43
Perigee (km) 2051
Apogee (km) 34012
Eccentricity 0.886254609988076
Mean motion (revs. per day) 2.27642790521207
Semi-Major axis (km) 24409.635
Raan (deg) 254.8536
Arg of perigee (deg) 278.6095
Shape Cyl
Mass (kg) 445.99
Diameter (m) 2.1
Height (m) 1.6
Span (m^2) 2.1
Equipment 2 C-band transponders
Propulsion FG-15B
Configuration DFH-2 Bus
Power Solar cells, batteries

China operated a constellation of three Dongfanghong DFH-2 (aka STTW = Shiyan Tongbu Tongxing Weixing) communications satellites in GEO for domestic needs. Designed, manufactured, and launched by indigenous means, the modest DFH-2 Dongfanghong DFH-2 (Dong Fang Hong - The East is Red) space craft were analogous to 1960's era Western GEO satellites (e.g., INTELSAT 3), although slightly heavier.

With an on-orbit mass of 441 kg (compared to 433 kg for the earlier satellites), DFH-2A spacecraft were successfully placed in GEO in March, 1988, December, 1988, and February, 1990, and positioned at 87.5 degrees E, 110.5 degrees E, and 98 degrees E, respectively. All three satellites remained on station at the end of 1994. A fourth DFH-2 was lost on 28 December 1991 when its CZ-3 upper stage failed to reignite. DFH-2A-1, 2A-2, 2A-3 were later renamed ChinaSat-1, ChinaSat-2 and ChinaSat-3, respectively.

The DFH-2A was a spin-stabilized, drum-shaped satellite with a diameter of 2.1 m and a height of 3.1 m. The communications payload consisted of only two 6/4 GHz transponders with an output power of 10 W. The total electrical power capacity was assessed to be about 300 W (the first two experimental satellites were rated at 284 W).

Prior to 1993 all DFH satellites were operated by the military. All DFH-2As had exhausted fuel and halted operation by the early 1990s.

Satellite COSPAR Date LS Launch Vehicle Remarks
STTW-1 1986-010A 1986-02-01 XSC CZ-3
STTW-2 1988-014A 1988-03-07 XSC CZ-3
STTW-3 1988-111A 1988-12-22 XSC CZ-3
STTW-4 1990-011A 1990-02-04 XSC CZ-3
STTW-5 1991-088A 1991-12-28 XSC CZ-3