ONEWEB-0063, 45448
Orbit data source: Space-Track
ONEWEB-0063, 45448 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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45448 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 ONEWEB-0063
1 45448U 20020AA 25286.43006476 -.00000497 00000-0 -14396-2 0 9999
2 45448 87.8816 70.1986 0001731 87.8724 272.2602 13.11415990270356
TLE epoch observation values (Epoch: 2025-10-13T10:19:17.595Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #20 in the year 2020 (2020-03-21 UTC)
ONEWEB-0063 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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14 mins | 2025-10-14 10:12:28.284Z | 181.438° SSW | 2025-10-14 10:19:28.284Z | 229.561° WSW | 44.725° | 2025-10-14 10:26:28.284Z | 359.069° N |
5 mins | 2025-10-14 12:08:28.284Z | 269.961° W | 2025-10-14 12:10:28.284Z | 287.045° WNW | 13.168° | 2025-10-14 12:13:28.284Z | 312.485° NW |
13 mins | 2025-10-14 21:43:28.284Z | 2.81° NNE | 2025-10-14 21:49:28.284Z | 89.322° E | 44.525° | 2025-10-14 21:56:28.284Z | 176.167° S |
7 mins | 2025-10-14 23:35:28.284Z | 314.58° NW | 2025-10-14 23:38:28.284Z | 286.798° WNW | 16.934° | 2025-10-14 23:42:28.284Z | 251.796° W |
5 mins | 2025-10-15 08:17:28.284Z | 86.659° E | 2025-10-15 08:19:28.284Z | 68.859° E | 14.035° | 2025-10-15 08:22:28.284Z | 43.665° NE |
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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