ONEWEB-0052, 45156
Orbit data source: Space-Track
ONEWEB-0052, 45156 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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45156 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-0052
1 45156U 20008AB 25255.81120434 -.00000532 00000-0 -15591-2 0 9998
2 45156 87.8754 91.5532 0002258 86.8851 273.2535 13.10374246271615
TLE epoch observation values (Epoch: 2025-09-12T19:28:08.054Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #8 in the year 2020 (2020-02-06 UTC)
ONEWEB-0052 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 11:55:41.282Z | 112.406° ESE | 2025-09-14 11:59:41.282Z | 78.158° E | 17.787° | 2025-09-14 12:04:41.282Z | 33.955° NE |
12 mins | 2025-09-14 13:43:41.282Z | 187.542° SSW | 2025-09-14 13:49:41.282Z | 302.359° NW | 43.808° | 2025-09-14 13:55:41.282Z | 356.515° N |
5 mins | 2025-09-14 23:26:41.282Z | 54.931° ENE | 2025-09-14 23:28:41.282Z | 72.763° E | 14.213° | 2025-09-14 23:31:41.282Z | 98.376° ESE |
13 mins | 2025-09-15 01:13:41.282Z | 359.992° N | 2025-09-15 01:19:41.282Z | 153.758° SSE | 44.957° | 2025-09-15 01:26:41.282Z | 180.842° SSW |
6 mins | 2025-09-15 03:05:41.282Z | 312.858° NW | 2025-09-15 03:08:41.282Z | 286.369° WNW | 14.892° | 2025-09-15 03:11:41.282Z | 260.65° 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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