ONEWEB-0596, 54662
Orbit data source: Space-Track
ONEWEB-0596, 54662 is a payload satellite owned by One Web (NAA) (UK) in LEO that was launched on Thu, 08 Dec 2022 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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54662 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: 2 days ago
TLE from 2 days ago
0 ONEWEB-0596
1 54662U 22166W 26171.18262813 .00000023 00000-0 24699-4 0 9997
2 54662 87.9253 243.3885 0002072 101.0012 259.1355 13.21826643171935Epoch: 2026-06-20T04:22Z
TLE epoch observation values (Epoch: 2026-06-20T04:22:59.070Z)
Latitude
-0.00003°
Longitude
-90.75854°
Altitude
1,180.951 km
Speed
7.263 km/s
True Right ascension
16h 13m 33s
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
21:32:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,176.418 km
Perigee altitude
1,173.288 km
Semi-major axis
7,552.99 km
Eccentricity
0.00021
Inclination
87.9253°
RAAN
243.3885°
Arg. of periapsis
101.0012°
True anomaly
259.11218°
Mean anomaly
259.1355°
Eccentric anomaly
259.12384°
Mean motion
3.30647 °/min
Orbital period
108.88 mins
BSTAR
0.000024699
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Other satellites on launch #166 in the year 2022 (2022-12-08 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-0596 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-22 15:08:45.692Z | 40.225° NE | 2026-06-22 15:12:45.692Z | 74.943° E | 14.314° | 2026-06-22 15:15:45.692Z | 101.042° ESE |
| 12 mins | 2026-06-22 16:56:45.692Z | 359.229° N | 2026-06-22 17:02:45.692Z | 190.104° SSW | 44.786° | 2026-06-22 17:08:45.692Z | 182.111° SSW |
| 5 mins | 2026-06-22 18:48:45.692Z | 303.46° NW | 2026-06-22 18:50:45.692Z | 285.154° WNW | 13.883° | 2026-06-22 18:53:45.692Z | 259.749° W |
| 6 mins | 2026-06-23 03:24:45.692Z | 93.649° ESE | 2026-06-23 03:26:45.692Z | 75.574° E | 14.699° | 2026-06-23 03:30:45.692Z | 40.576° NE |
| 12 mins | 2026-06-23 05:09:45.692Z | 180.265° SSW | 2026-06-23 05:14:45.692Z | 197.581° SSW | 44.668° | 2026-06-23 05:21:45.692Z | 359.892° N |
| 4 mins | 2026-06-23 07:03:45.692Z | 275.517° WNW | 2026-06-23 07:04:45.692Z | 284.527° WNW | 13.473° | 2026-06-23 07:07:45.692Z | 311.072° NW |
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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