ONEWEB-0054, 45158
Orbit data source: Space-Track
ONEWEB-0054, 45158 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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45158 intel report (Beta)
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Identifier
Orbit
Country
UKRelated business
Manufacturer
One Web
Mission
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: 13 hours ago
TLE from 13 hours ago
0 ONEWEB-0054
1 45158U 20008AD 26272.08180731 -.00000523 00000-0 -15342-2 0 9999
2 45158 87.8905 15.5928 0001772 104.0211 256.1113 13.10370385321633Epoch: 2026-09-29T01:57Z
TLE epoch observation values (Epoch: 2026-09-29T01:57:48.151Z)
Latitude
-0.00007°
Longitude
-21.70976°
Altitude
1,224.938 km
Speed
7.242 km/s
True Right ascension
01h 02m 22s
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
08:10:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,220.192 km
Perigee altitude
1,217.5 km
Semi-major axis
7,596.983 km
Eccentricity
0.00018
Inclination
87.8905°
RAAN
15.5928°
Arg. of periapsis
104.0211°
True anomaly
256.09159°
Mean anomaly
256.1113°
Eccentric anomaly
256.10144°
Mean motion
3.27779 °/min
Orbital period
109.83 mins
BSTAR
-0.0015342
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Other satellites on launch #8 in the year 2020 (2020-02-06 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-0054 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-29 17:16:32.257Z | 50.002° ENE | 2026-09-29 17:18:32.257Z | 66.235° ENE | 12.059° | 2026-09-29 17:21:32.257Z | 90.753° ESE |
| 13 mins | 2026-09-29 19:04:32.257Z | 4.134° NNE | 2026-09-29 19:10:32.257Z | 120.179° SE | 75.144° | 2026-09-29 19:17:32.257Z | 175.229° S |
| 8 mins | 2026-09-29 20:55:32.257Z | 320.259° NNW | 2026-09-29 20:59:32.257Z | 283.779° WNW | 18.46° | 2026-09-29 21:03:32.257Z | 249.231° W |
| 5 mins | 2026-09-30 05:38:32.257Z | 87.015° E | 2026-09-30 05:40:32.257Z | 69.524° E | 14.201° | 2026-09-30 05:43:32.257Z | 44.468° NE |
| 13 mins | 2026-09-30 07:23:32.257Z | 176.094° S | 2026-09-30 07:29:32.257Z | 31.884° NE | 82.581° | 2026-09-30 07:36:32.257Z | 1.677° NNE |
| 6 mins | 2026-09-30 09:17:32.257Z | 264.187° W | 2026-09-30 09:20:32.257Z | 291.43° WNW | 16.034° | 2026-09-30 09:23:32.257Z | 317.384° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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