China Direct Broadcast Satellite Company Ltd. (China DBSAT)

SINOSAT
Satellite name: Sinosat-1,110.5°E; Sinosat-3,125°E; Sinosat-4, 92.2°E*; Sinosat-5, 110.5°E*; Sinosat-6,125°E
Spacecraft data:
Model: Spacebus-3000 (1), DFH-3 (3), DFH-4 (4)
Area of coverage: China and Asia Pacific areas (C-band); China and neighboring areas (Ku-band) [1]; China and neighboring areas [3, 4]
Mass (in orbit): 1,600 kg
Primary power (EOL): 5,300 W
Stabilization: 3-axis
Launch datę: July 18,1998 (1); June 1, 2007 (3); Late 2011 (4); 2011 (5); September5, 2010 (6)
Launch vehicle: Long March 3B (1, 6); Long March 3A (3)
Expected lifetime: 15 years (1,4, 5, 6); 8 years (3)
Transponders:
Number: 24 C-band @ 21 W,14 Ku-band @ 97 W (1); 10 C-band (3); 24 C-band, 8 Ku-band, 1 S-band (6)
Uplink frequency: 5.825-6.425 GHz (C-band); 14.00-14.50 GHz (Ku-band) [1]; 5.925-6.425 GHz [3]
Downlinkfrequency: 3625-4200 MHz (C-band); 12.25-12.75 GHz (Ku-band) [1]; 3.7 – 4.2 GHz [3]
Polarization: Linear
Redundancy: 4:2 receiver
G/T: -3 dB/K (C-band), 0-6 dB/K (Ku-band) [1 ]; > 0.0 dB/K (3)
Bandwidth: 23 @ 36 MHz, 1 @ 54 MHz (C-band), 54 MHz (Ku-band) [1 ]; 36 MHz (3)
EIRP: 36 dBW (C-band), 46 to 52 dBW (Ku-band) [1 ]; China > 40 dBW, SE Asia & neighboring regions > 36 dBW (3)
Single carrier saturation flux density: -70 to -98 dBW/m2 (C-band), -70 to -98 (FGM), -70 to -90 (ALC) dBW/m2 (Ku-band) [1];-75 to-98 dBW/m2 (FGM), -75 to -90 dBW/m2 (ALC) [3]
Manufacturer: Alcatel Space (formerly Aerospatiale) [1 ], China Academy of Space Tech­nology (3)
*To be launched

 

► CHINASAT

Satellite name: ChinaSat-9, 92.2°E; ChinaSat-6B, 115.5°E

Spacecraft data:

Model: Spacebus 4000 C2

Mass (at launch) 4,500 kg

Coverage: China, SE Asia, NE Asia, S. Asia, Central Asia, W. Asia, Australia, New Zealand

Primary power: 11,000 W (9)

Stabilization: 3-axis

Launch date: June 9, 2008 (9); July 5, 2007 (6B)

Launch vehicle: Long March 3B

Expected lifetime: 15 years

Transponders:

Number: 22 Ku-band (9); 38 C-band (6B)

Bandwidth 18 @ 36 MHz, 4 @ 54 MHz (9)

Polarization: Linear (6B); Circular (9)

Uplink frequency: 5850 – 6665 MHz (6B), 17.3 -17.8 GHz (9)

D/L frequency: 3400 -4200 MHz (6B), 11.7 -12.2 GHz (9)

G/T: 1.5 dB/K (6B), 0.0 dB/K (9)

Manufacturer: Thales Alenia Space

 

CHINASTAR
Satellite name:               | ChinaStar-1, 87.5°E; ChinaStar-2, 87.5°E (to be launched)
Spacecraft data:
Model: LM A2100A (1)
Mass (at launch) 1,418 kg (1)
Coverage: China (including Hong Kong, Macao and Taiwan), South, West, East, Central and Southeast Asia
Primary power: 7,665 W (spring equinox BOL), 6,940 W (autumn equinox EOL) (1)
Stabilization: 3-axis
Launch datę: May 31,1998 (1); TBA(2)
Launch vehicle: Long March 3B (1)
Expected lifetime: 15 years
Transponders:
Number: 18 C-band, 20 Ku-band (1)
Power output 45 W (1)
Bandwidth 12 @ 36 MHz, 6 @ 72 MHz (C-band),16 @ 36 MHz, 4 @ 72 MHz (Ku-band) (1)
Polarization: Linear
Uplink frequency: 5925-6425 MHz (C-band), 14000-14500 MHz (Ku-band) (1)
D/L frequency: 3700-4200 MHz (C-band), 12250-12750 MHz (Ku-band) (1)
G/T: +2.91 dB/K (C-band), +9.79 dB/K (Ku-band) (1)
EIRP: 44.06 dBW (C-band), 54.19 dBW (36 MHz), 55.95 dBW (72 MHz) [Ku-band] (1)
SCSFD: -75 to -97 dBW/m2 (C-band), -70 to -92 dBW/m2 (Ku-band) (1)
Manufacturer: Lockheed Martin (1)