ONEWEB-0057, 45160
Orbit data source: Space-Track
ONEWEB-0057, 45160 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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45160 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-0057
1 45160U 20008AF 25255.96972694 -.00000370 00000-0 -10959-2 0 9995
2 45160 87.8741 91.5596 0001812 82.3232 277.8101 13.10375727272047
TLE epoch observation values (Epoch: 2025-09-12T23:16:24.407Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #8 in the year 2020 (2020-02-06 UTC)
ONEWEB-0057 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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9 mins | 2025-09-14 12:03:40.956Z | 117.598° SE | 2025-09-14 12:08:40.956Z | 71.42° E | 20.248° | 2025-09-14 12:12:40.956Z | 34.573° NE |
13 mins | 2025-09-14 13:51:40.956Z | 192.712° SSW | 2025-09-14 13:57:40.956Z | 274.691° WNW | 42.588° | 2025-09-14 14:04:40.956Z | 354.885° N |
7 mins | 2025-09-14 23:33:40.956Z | 42.537° NE | 2025-09-14 23:36:40.956Z | 69.236° E | 16.371° | 2025-09-14 23:40:40.956Z | 105.227° ESE |
13 mins | 2025-09-15 01:21:40.956Z | 356.943° N | 2025-09-15 01:27:40.956Z | 299.694° NW | 44.607° | 2025-09-15 01:34:40.956Z | 185.957° SSW |
4 mins | 2025-09-15 03:14:40.956Z | 306.71° NW | 2025-09-15 03:16:40.956Z | 289.733° WNW | 12.801° | 2025-09-15 03:18:40.956Z | 272.797° WNW |
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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