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BEIDOU-3 M8 (43108)
COSPAR: 2018-003B | Alt Name: Beidou DW 27
Image
Additional Sources
Launch Details
Launch Date
January 11, 2018
Launch Site
XICLF
Launch Pad
LC3
Launch Vehicle
Chang Zheng 3B/YZ-1
Orbital Elements
NORAD ID
43108
International Designator
2018-003B
Epoch
Fri, 03 Jul 2026 22:34:48 GMT
Apogee
Calculating...
Perigee
Calculating...
Inclination
54.30°
Right Ascension
301.71°
Eccentricity
Calculating...
Argument of Perigee
257.96°
Period
773.23 min
Mean Motion
1.86 rev/day
Latitude
Calculating...
Longitude
Calculating...
Altitude
Calculating...
Velocity
Calculating...
Polar Plot
3D Visualization
Basic Satellite Info
Name
BEIDOU-3 M8
Alternative Name
Beidou DW 27
Type
Payload
Status
Operational
Owner
CNSA
Country
China
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 43108U 18003B 26184.94083422 -.00000059 00000-0 00000-0 0 9996
2 43108 54.3045 301.7129 0002939 257.9576 102.0322 1.86231143 57670
Source: Celestrak
Summary
BEIDOU-3 M8, also known as Beidou DW 27, is a navigation satellite launched on January 11, 2018, from Xichang Satellite Launch Center (XICLF), using the Chang Zheng 3B/YZ-1 launch vehicle. The spacecraft has dimensions of 2.2 meters in length and 1.7 meters in diameter with a span of 10 meters. It features two deployable solar arrays and batteries for power generation. The satellite's dry mass is 850 kilograms, and it was launched with a total mass of 1014 kilograms. Manufactured by SECM (Satellite Equipment & Component Manufacturing), BEIDOU-3 M8 operates under the ownership of CNSA (China National Space Administration) for navigation purposes as part of the Beidou satellite system, designed to provide precise global positioning services with an expected operational lifetime of 12 years.
Physical Characteristics
Length
2.2
Diameter
1.7
Span
10
Dry Mass
850
Launch Mass
1014
Shape
Box + 2 Pan
Radar Cross Section
Unknown
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
Beidou-3 M8
Purpose
Navigation
Mission
Navigation
Manufacturer
SECM
Life Expectancy
12 years
Bus
BD-3M2
Configuration
Unknown
Motor
Unknown
Equipment
?
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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