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ONEWEB-0613 (56071)
COSPAR: 2023-043AB | Alt Name: OneWeb SL0613
Image
Additional Sources
Launch Details
Launch Date
March 26, 2023
Launch Site
SRILR
Launch Pad
SLP
Launch Vehicle
LVM3
Orbital Elements
NORAD ID
56071
International Designator
2023-043AB
Epoch
Sun, 19 Jul 2026 04:46:46 GMT
Apogee
Calculating...
Perigee
Calculating...
Inclination
87.90°
Right Ascension
252.84°
Eccentricity
Calculating...
Argument of Perigee
102.62°
Period
109.46 min
Mean Motion
13.16 rev/day
Latitude
Calculating...
Longitude
Calculating...
Altitude
Calculating...
Velocity
Calculating...
Polar Plot
3D Visualization
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Basic Satellite Info
Name
ONEWEB-0613
Alternative Name
OneWeb SL0613
Type
Payload
Status
Operational
Owner
ONEWEBN
Country
United Kingdom
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 56071U 23043AB 26200.19914478 .00000116 00000+0 27303-3 0 9999
2 56071 87.8976 252.8449 0002211 102.6179 257.5199 13.15548007160641
Source: Celestrak
Summary
The ONEWEB-0613 satellite, also known as OneWeb SL0613, was launched on March 26, 2023, from the Sriharikota Launch Range using a LVM3 launch vehicle. It has an arrow bus configuration with dimensions of 1.3 meters in length and 1 meter in diameter, with solar arrays providing power storage in batteries. The satellite's dry mass is 140 kilograms, while its launch mass was 148 kilograms. Equipped with a Ku-Band payload for communication purposes, it uses SPT-50 or BHT-350 Hall effect thrusters as motors and has an expected operational lifetime of seven years. The satellite's shape is described as Trapezoid+2 pan, and its mission focuses on providing communication services. It was manufactured by ONEWUS and is owned by ONEWEBN.
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 L18-026
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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Two-Line Element Set (TLE)
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