ONEWEB-0080, 45426
Orbit data source: Space-Track
ONEWEB-0080, 45426 is a payload satellite owned by One Web (UK) in LEO that was launched on Sat, 21 Mar 2020 UTC via a SOYUZ-2-1B launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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45426 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
UKRelated business
Manufacturer
One Web
Mission
Operational Commercial Communications
Bus & Motor
ARROW, Unknown motor
Mass
148 kg wet, ~140 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trap Box + 2 Pan, 6.7 m
Radar Cross Section
3.464 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 ONEWEB-0080
1 45426U 20020C 26035.05546690 .00000795 00000-0 22083-2 0 9994
2 45426 87.8815 47.5547 0001608 99.4544 260.6766 13.11420074285250Epoch: 2026-02-04T01:19Z
TLE epoch observation values (Epoch: 2026-02-04T01:19:52.340Z)
Latitude
0.00002°
Longitude
-106.64092°
Altitude
1,220.758 km
Speed
7.244 km/s
True Right ascension
03h 10m 13s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
14:17:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.01 km
Perigee altitude
1,213.568 km
Semi-major axis
7,592.926 km
Eccentricity
0.00016
Inclination
87.8815°
RAAN
47.5547°
Arg. of periapsis
99.4544°
True anomaly
260.65842°
Mean anomaly
260.6766°
Eccentric anomaly
260.66751°
Mean motion
3.28042 °/min
Orbital period
109.74 mins
BSTAR
0.0022083
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Other satellites on launch #20 in the year 2020 (2020-03-21 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ONEWEB-0080 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2026-02-04 12:55:16.102Z | 0.271° NNE | 2026-02-04 13:02:16.102Z | 163.046° S | 44.516° | 2026-02-04 13:08:16.102Z | 179.781° S |
| 6 mins | 2026-02-04 14:48:16.102Z | 309.52° NW | 2026-02-04 14:50:16.102Z | 291.584° WNW | 15.211° | 2026-02-04 14:54:16.102Z | 257.024° W |
| 6 mins | 2026-02-04 23:29:16.102Z | 91.863° ESE | 2026-02-04 23:31:16.102Z | 73.492° E | 15.669° | 2026-02-04 23:35:16.102Z | 39.062° NE |
| 13 mins | 2026-02-05 01:14:16.102Z | 181.466° SSW | 2026-02-05 01:20:16.102Z | 262.861° W | 44.889° | 2026-02-05 01:27:16.102Z | 359.459° N |
| 5 mins | 2026-02-05 03:09:16.102Z | 271.651° WNW | 2026-02-05 03:11:16.102Z | 289.017° WNW | 13.412° | 2026-02-05 03:14:16.102Z | 314.32° NW |
| 4 mins | 2026-02-05 10:57:16.102Z | 55.771° ENE | 2026-02-05 10:59:16.102Z | 72.604° E | 12.015° | 2026-02-05 11:01:16.102Z | 89.086° E |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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