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APSTAR-6D (45863)
COSPAR: 2020-045A | Alt Name: Apstar 6D
Image
Additional Sources
Launch Details
Launch Date
July 9, 2020
Launch Site
XICLF
Launch Pad
LC3
Launch Vehicle
Chang Zheng 3B
Orbital Elements
NORAD ID
45863
International Designator
2020-045A
Epoch
Sat, 04 Jul 2026 04:27:38 GMT
Apogee
Calculating...
Perigee
Calculating...
Inclination
0.05°
Right Ascension
91.43°
Eccentricity
Calculating...
Argument of Perigee
352.42°
Period
1436.04 min
Mean Motion
1.00 rev/day
Latitude
Calculating...
Longitude
Calculating...
Altitude
Calculating...
Velocity
Calculating...
Polar Plot
3D Visualization
Basic Satellite Info
Name
APSTAR-6D
Alternative Name
Apstar 6D
Type
Payload
Status
Operational
Owner
APTS
Country
China
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 45863U 20045A 26185.18586492 -.00000305 00000-0 00000-0 0 9991
2 45863 0.0453 91.4256 0002210 352.4150 39.3098 1.00275826 22032
Source: Celestrak
Summary
APSTAR-6D, also known as Apstar 6D, is a communication satellite manufactured by CAST and owned by APTS. Launched on July 9, 2020, from Xichang Satellite Launch Center (XICLF) using the Chang Zheng 3B launch vehicle, it uses the DFH-4E Bus configuration and carries a Ka-band high throughput communications payload. The satellite has dimensions of 5 meters in length, 2.5 meters in diameter, and a span of 30 meters when deployed. It weighs 5000 kilograms at launch with a dry mass of 2500 kilograms. APSTAR-6D is powered by two deployable solar arrays and batteries and has a projected lifetime of 15 years. The satellite's shape consists of a box design with two panels, and its purpose is to provide communication services.
Physical Characteristics
Length
5
Diameter
2.5
Span
30
Dry Mass
2500
Launch Mass
5000
Shape
Box+ 2 pan
Radar Cross Section
Unknown
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
Apstar 6D
Purpose
Communication
Mission
Communication
Manufacturer
CAST
Life Expectancy
15 years
Bus
DFH-4E
Configuration
DFH-4E Bus
Motor
DFH-4 LAE
Equipment
Ka-band high throughput communications payload
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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