ONEWEB-0054, 45158
Orbit data source: Space-Track
ONEWEB-0054, 45158 is a payload satellite owned by One Web (UK) in LEO that was launched on Thu, 06 Feb 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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45158 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ONEWEB-0054
1 45158U 20008AD 25255.98135501 .00000215 00000-0 57870-3 0 9992
2 45158 87.8744 91.5460 0001741 87.4803 272.6524 13.10376183271721
TLE epoch observation values (Epoch: 2025-09-12T23:33:09.072Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #8 in the year 2020 (2020-02-06 UTC)
ONEWEB-0054 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. |
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13 mins | 2025-09-14 01:48:45.230Z | 349.696° N | 2025-09-14 01:54:45.230Z | 288.3° WNW | 39.907° | 2025-09-14 02:01:45.230Z | 200.297° SSW |
10 mins | 2025-09-14 12:20:45.230Z | 122.283° SE | 2025-09-14 12:24:45.230Z | 79.411° E | 25.593° | 2025-09-14 12:30:45.230Z | 22.961° NE |
12 mins | 2025-09-14 14:08:45.230Z | 204.847° SW | 2025-09-14 14:14:45.230Z | 283.303° WNW | 37.751° | 2025-09-14 14:20:45.230Z | 348.234° N |
9 mins | 2025-09-14 23:49:45.230Z | 33.951° NE | 2025-09-14 23:53:45.230Z | 72.136° E | 21.273° | 2025-09-14 23:58:45.230Z | 120.39° SE |
4 mins | 2025-09-15 01:38:45.230Z | 350.424° N | 2025-09-15 01:42:45.230Z | 327.057° NNW | 37.083° | 2025-09-15 01:42:45.230Z | 327.057° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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