Official name CHINASAT 22A
Alternative name Chinasat 22A
Cospar ID 2006-038A
Norad ID 29398
Launch date 2006-09-12
Launch site XSC
Launch vehicle CZ-3A
Country/Organization China
Type application Communication
Operator People's Liberation Army (PLA)
RCS size LARGE
Decay date ON ORBIT
Period (min) 1438.56
Inclination (deg) 10.09
Perigee (km) 35817
Apogee (km) 35852
Eccentricity 0.00048835619305418
Mean motion (revs. per day) 1.001001001001
Semi-Major axis (km) 42212.635
Raan (deg) 43.3006
Arg of perigee (deg) 53.841
Shape Box + 2 Pan
Mass (kg) 2300
Height (m) 5.7
Width (m) 1.7
Depth (m) 1.7
Span (m^2) 18.1
Lifetime 8 years
Contractors CAST
Equipment C-band and UHF transponders
Propulsion ?
Configuration DFH-3 Bus
Power 2 deployable solar arrays, batteries

The FH 1 (Feng Huo 1) series are reportedly chinese military comsats and data relay satellites. They provide both C-band and UHF communications.

China Aerospace Science and Technology Corp. manufactured the satellites based on the DFH-3 Bus. The launch vehicle was the CZ-3A rocket.

The first of these satellites, FH 1A was launched in January 2001 and was given the designation ZX 22 (ChinaSat 22).

A second satellite FH 1B or ZX 22A (ChinaSat 22A) followed in September 2006.

Satellite COSPAR Date LS Launch Vehicle Remarks
CHINASAT 22 2000-003A 2000-01-25 XSC CZ-3A
CHINASAT 22A 2006-038A 2006-09-12 XSC CZ-3A