ONEWEB-0050, 45453
Orbit data source: Space-Track
ONEWEB-0050, 45453 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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45453 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
UKRelated business
Manufacturer
One Web
Mission
Partially operational Commercial Communications
Bus & Motor
ARROW, Unknown motor
Mass
148 kg wet, ~140 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trap Box + 2 Pan, 6.7 m
Radar Cross Section
3.464 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 ONEWEB-0050
1 45453U 20020AF 26035.51277399 .00002372 00000-0 24470-3 0 9998
2 45453 88.9193 251.2995 0005814 90.2118 269.9777 14.89867588320627Epoch: 2026-02-04T12:18Z
TLE epoch observation values (Epoch: 2026-02-04T12:18:23.672Z)
Latitude
-0.00004°
Longitude
-67.97742°
Altitude
601.505 km
Speed
7.559 km/s
True Right ascension
16h 45m 11s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
01:37:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
599.256 km
Perigee altitude
591.147 km
Semi-major axis
6,973.338 km
Eccentricity
0.00058
Inclination
88.9193°
RAAN
251.2995°
Arg. of periapsis
90.2118°
True anomaly
269.91108°
Mean anomaly
269.9777°
Eccentric anomaly
269.94439°
Mean motion
3.72719 °/min
Orbital period
96.59 mins
BSTAR
0.0002447
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Other satellites on launch #20 in the year 2020 (2020-03-21 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ONEWEB-0050 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-05 01:46:48.758Z | 35.963° NE | 2026-02-05 01:49:48.758Z | 88.168° E | 21.013° | 2026-02-05 01:52:48.758Z | 134.944° SE |
| 5 mins | 2026-02-05 03:23:48.758Z | 324.629° NNW | 2026-02-05 03:25:48.758Z | 288.598° WNW | 23.265° | 2026-02-05 03:28:48.758Z | 230.871° WSW |
| 6 mins | 2026-02-05 14:13:48.758Z | 146.183° SSE | 2026-02-05 14:16:48.758Z | 78.54° E | 32.536° | 2026-02-05 14:19:48.758Z | 19.38° NNE |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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