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ONEWEB-0032 (45141)
COSPAR: 2020-008L | Alt Name: OneWeb SL0032
Image
Additional Sources
Launch Details
Launch Date
February 6, 2020
Launch Site
Launch Pad
LC31
Launch Vehicle
Soyuz-2-1B
Orbital Elements
NORAD ID
45141
International Designator
2020-008L
Epoch
Sat, 04 Jul 2026 00:42:14 GMT
Apogee
Calculating...
Perigee
Calculating...
Inclination
87.88°
Right Ascension
32.91°
Eccentricity
Calculating...
Argument of Perigee
69.87°
Period
109.89 min
Mean Motion
13.10 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
ONEWEB-0032
Alternative Name
OneWeb SL0032
Type
Payload
Status
Operational
Owner
ONEWEB
Country
United Kingdom
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 45141U 20008L 26185.02933633 .00000659 00000-0 18525-2 0 9999
2 45141 87.8818 32.9145 0001703 69.8729 290.2582 13.10372948310508
Source: Celestrak
Summary
The ONEWEB-0032 satellite, also known as OneWeb SL0032, was launched on February 6, 2020, from the TYMSC launch site using a Soyuz-2-1B vehicle from Launch Pad LC31. This communication satellite uses an Arrow bus configuration and is owned by ONEWEB. It has dimensions of 1.3 meters in length, 1 meter in diameter, and a span of 5 meters. The satellite's dry mass is 140 kilograms with a launch mass of 148 kilograms. It features a Ku-Band payload for communication purposes and is powered by solar arrays and batteries. ONEWEB-0032 has a trapezoidal shape complemented by two panels and is equipped with SPT-50 or BHT-350 Hall effect thrusters as its motor system. The expected operational lifetime of the satellite is 7 years. It was manufactured by ONEWUS for the purpose of enhancing communication capabilities in orbit.
Physical Characteristics
Length
1.3
Diameter
1
Span
5
Dry Mass
140
Launch Mass
148
Shape
Trapezoid+2 pan
Radar Cross Section
Unknown
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
OneWeb L2-009
Purpose
Communication
Mission
Communication
Manufacturer
ONEWUS
Life Expectancy
+ 7 years
Bus
ARROW
Configuration
Arrow bus
Motor
SPT-50 or BHT-350 Hall effect thrusters
Equipment
Ku-Band payload
Power System
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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