ONEWEB-0056, 45159
Orbit data source: Space-Track
ONEWEB-0056, 45159 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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45159 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 ONEWEB-0056
1 45159U 20008AE 25256.26768278 -.00000720 00000-0 -20988-2 0 9990
2 45159 87.8740 91.4862 0001708 85.7107 274.4215 13.10373496271916
TLE epoch observation values (Epoch: 2025-09-13T06:25:27.792Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #8 in the year 2020 (2020-02-06 UTC)
ONEWEB-0056 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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8 mins | 2025-09-14 11:53:56.743Z | 107.2° ESE | 2025-09-14 11:57:56.743Z | 71.482° E | 17.176° | 2025-09-14 12:01:56.743Z | 36.703° NE |
13 mins | 2025-09-14 13:40:56.743Z | 185.315° SSW | 2025-09-14 13:46:56.743Z | 279.363° WNW | 44.429° | 2025-09-14 13:53:56.743Z | 357.982° N |
5 mins | 2025-09-14 23:23:56.743Z | 52.329° ENE | 2025-09-14 23:25:56.743Z | 69.624° E | 13.572° | 2025-09-14 23:28:56.743Z | 95.184° ESE |
13 mins | 2025-09-15 01:10:56.743Z | 0.772° NNE | 2025-09-15 01:16:56.743Z | 45.703° ENE | 44.837° | 2025-09-15 01:23:56.743Z | 179.202° S |
6 mins | 2025-09-15 03:03:56.743Z | 307.901° NW | 2025-09-15 03:05:56.743Z | 289.64° WNW | 15.57° | 2025-09-15 03:09:56.743Z | 255.335° W |
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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