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ZHONGXING-22A (29398)
COSPAR: 2006-038A | Alt Name: Zhongxing 22A
Image
Additional Sources
Launch Details
Launch Date
September 12, 2006
Launch Site
XICLF
Launch Pad
LC2
Launch Vehicle
Chang Zheng 3A
Orbital Elements
NORAD ID
29398
International Designator
2006-038A
Epoch
Fri, 03 Jul 2026 21:32:58 GMT
Apogee
Calculating...
Perigee
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Inclination
11.52°
Right Ascension
37.21°
Eccentricity
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Argument of Perigee
109.97°
Period
1438.44 min
Mean Motion
1.00 rev/day
Latitude
Calculating...
Longitude
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Altitude
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Velocity
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Polar Plot
3D Visualization
Basic Satellite Info
Name
ZHONGXING-22A
Alternative Name
Zhongxing 22A
Type
Payload
Status
Non-operational
Owner
ZZB
Country
China
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 29398U 06038A 26184.89790462 -.00000120 00000-0 00000-0 0 9998
2 29398 11.5210 37.2083 0002869 109.9656 261.4931 1.00108272 72553
Source: Celestrak
Summary
ZHONGXING-22A, also known as Zhongxing 22A, is a communication satellite manufactured by CAST and launched on September 12, 2006, from Xichang Satellite Launch Center (LC2) using the Chang Zheng 3A launch vehicle. With a dry mass of 1100 kg and a launch mass of 2330 kg, it is equipped with C-band and UHF transponders for communication purposes. The satellite's dimensions include a length of 5.7 meters, diameter of 1.7 meters, and span of 18.1 meters. It features 2 deployable solar arrays and batteries for power generation. ZHONGXING-22A has an expected lifetime of 8 years and carries the Fenghuo-1 02 xing payload. The satellite's shape is described as a box with two panels, and it has a radar cross-section (RCS) value of 18.8988 square meters. It operates in the DFH-3 Bus configuration and was launched for ZZB, the owner entity.
Physical Characteristics
Length
5.7
Diameter
1.7
Span
18.1
Dry Mass
1100
Launch Mass
2330
Shape
Box + 2 Pan
Radar Cross Section
18.8988
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
Fenghuo-1 02 xing
Purpose
Communication
Mission
Communication
Manufacturer
CAST
Life Expectancy
8 years
Bus
DFH-3
Configuration
DFH-3 Bus
Motor
FY-25
Equipment
C-band and UHF transponders
Power System
2 deployable solar arrays, batteries
ADCS
Unknown
Transmitter Frequency
Unknown
Map
Next Pass
Azimuth Elevation Time (Local)
Start Azimuth
Max Elevation
Stop Azimuth
Time Until
Pass Duration
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