ONEWEB-0591, 54657
Orbit data source: Space-Track
ONEWEB-0591, 54657 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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54657 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-0591
1 54657U 22166R 26171.26169560 -.00000049 00000-0 -14986-3 0 9992
2 54657 87.9250 243.3743 0002088 97.8801 262.2570 13.21825920171968Epoch: 2026-06-20T06:16Z
TLE epoch observation values (Epoch: 2026-06-20T06:16:50.499Z)
Latitude
-0.00004°
Longitude
-119.31497°
Altitude
1,180.871 km
Speed
7.263 km/s
True Right ascension
16h 13m 29s
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
21:26:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,176.433 km
Perigee altitude
1,173.279 km
Semi-major axis
7,552.993 km
Eccentricity
0.00021
Inclination
87.925°
RAAN
243.3743°
Arg. of periapsis
97.8801°
True anomaly
262.23329°
Mean anomaly
262.257°
Eccentric anomaly
262.24515°
Mean motion
3.30647 °/min
Orbital period
108.88 mins
BSTAR
-0.00014986
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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-0591 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 15:13:38.900Z | 39.564° NE | 2026-06-22 15:17:38.900Z | 75.362° E | 15.635° | 2026-06-22 15:20:38.900Z | 102.517° ESE |
| 12 mins | 2026-06-22 17:01:38.900Z | 357.245° N | 2026-06-22 17:07:38.900Z | 224.345° SW | 44.525° | 2026-06-22 17:13:38.900Z | 185.316° SSW |
| 4 mins | 2026-06-22 18:53:38.900Z | 302.705° NW | 2026-06-22 18:54:38.900Z | 293.964° NW | 12.617° | 2026-06-22 18:57:38.900Z | 268.111° W |
| 6 mins | 2026-06-23 03:29:38.900Z | 94.344° ESE | 2026-06-23 03:31:38.900Z | 75.415° E | 16.046° | 2026-06-23 03:35:38.900Z | 39.471° NE |
| 12 mins | 2026-06-23 05:14:38.900Z | 183.975° SSW | 2026-06-23 05:19:38.900Z | 228.852° WSW | 44.42° | 2026-06-23 05:26:38.900Z | 358.362° N |
| 4 mins | 2026-06-23 07:08:38.900Z | 276.315° WNW | 2026-06-23 07:10:38.900Z | 293.792° NW | 12.22° | 2026-06-23 07:12:38.900Z | 310.647° 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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