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O3B FM8 (40082)
COSPAR: 2014-038D | Alt Name: O3b FM8
Image
Additional Sources
Launch Details
Launch Date
July 10, 2014
Launch Site
FRGUI
Launch Pad
ELS
Launch Vehicle
Soyuz-ST-B
Orbital Elements
NORAD ID
40082
International Designator
2014-038D
Epoch
Thu, 02 Jul 2026 02:58:29 GMT
Apogee
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Perigee
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Inclination
0.05°
Right Ascension
348.72°
Eccentricity
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Argument of Perigee
113.62°
Period
287.93 min
Mean Motion
5.00 rev/day
Latitude
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Longitude
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Altitude
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Velocity
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Polar Plot
3D Visualization
Basic Satellite Info
Name
O3B FM8
Alternative Name
O3b FM8
Type
Payload
Status
Operational
Owner
O3B
Country
United Kingdom
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 40082U 14038D 26183.12394999 -.00000017 00000-0 00000-0 0 9995
2 40082 0.0463 348.7213 0002771 113.6205 257.6884 5.00116149218695
Source: Celestrak
Summary
O3B FM8 is a communication satellite with the NORAD catalog ID 40082 and object ID 2014-038D. Launched on July 10, 2014, from ELS launch pad at FRGUI using a Soyuz-ST-B vehicle, it has a configuration of ELiTeBus-1000 and is part of the Prisma bus series. The satellite was manufactured by THALR for O3B Networks, designed to operate in orbit with a mission duration of 10 years.
O3B FM8 measures 4 meters in length, has a diameter of 2 meters, and its span reaches up to 12 meters when its solar arrays are deployed. It carries 12 Ka-Band transponders for communication purposes and is powered by two deployable solar arrays alongside batteries. The satellite's dry mass is 500 kg with a launch mass of 700 kg.
Its shape consists of a box trap design with an additional two pan configuration, offering a radar cross-section (RCS) value of 3.9905 m². The AOCS system used for attitude control on board is the LS-400. This satellite serves the purpose of communication within its operational lifetime.
Physical Characteristics
Length
4
Diameter
2
Span
12
Dry Mass
500
Launch Mass
700
Shape
Box trap+2 pan
Radar Cross Section
3.9905
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
O3b 8
Purpose
Communication
Mission
Communication
Manufacturer
THALR
Life Expectancy
10 years
Bus
Prisma
Configuration
ELiTeBus-1000
Motor
LS-400 AOCS
Equipment
12 Ka-Band 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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