ONEWEB-0602, 54666
Orbit data source: Space-Track
ONEWEB-0602, 54666 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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54666 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-0602
1 54666U 22166AA 26171.48120287 -.00000015 00000-0 -68024-4 0 9995
2 54666 87.9250 243.3454 0001747 96.4742 263.6591 13.21826772171983Epoch: 2026-06-20T11:32Z
TLE epoch observation values (Epoch: 2026-06-20T11:32:55.927Z)
Latitude
-0.00004°
Longitude
161.41716°
Altitude
1,180.801 km
Speed
7.263 km/s
True Right ascension
16h 13m 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
21:41:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,176.172 km
Perigee altitude
1,173.533 km
Semi-major axis
7,552.99 km
Eccentricity
0.00017
Inclination
87.925°
RAAN
243.3454°
Arg. of periapsis
96.4742°
True anomaly
263.6392°
Mean anomaly
263.6591°
Eccentric anomaly
263.64915°
Mean motion
3.30647 °/min
Orbital period
108.88 mins
BSTAR
-0.000068024
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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-0602 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 | 2026-06-22 15:03:15.479Z | 45.38° ENE | 2026-06-22 15:06:15.479Z | 70.803° E | 12.76° | 2026-06-22 15:09:15.479Z | 96.278° ESE |
| 13 mins | 2026-06-22 16:50:15.479Z | 1.4° NNE | 2026-06-22 16:56:15.479Z | 68.877° E | 44.794° | 2026-06-22 17:03:15.479Z | 178.334° S |
| 6 mins | 2026-06-22 18:42:15.479Z | 308.112° NW | 2026-06-22 18:44:15.479Z | 289.331° WNW | 15.571° | 2026-06-22 18:48:15.479Z | 254.15° W |
| 5 mins | 2026-06-23 03:19:15.479Z | 87.949° E | 2026-06-23 03:21:15.479Z | 70.291° E | 13.161° | 2026-06-23 03:24:15.479Z | 44.81° NE |
| 12 mins | 2026-06-23 05:03:15.479Z | 175.752° S | 2026-06-23 05:09:15.479Z | 53.587° ENE | 44.846° | 2026-06-23 05:15:15.479Z | 1.911° NNE |
| 6 mins | 2026-06-23 06:56:15.479Z | 262.132° W | 2026-06-23 06:59:15.479Z | 289.744° WNW | 15.137° | 2026-06-23 07:02:15.479Z | 316.499° 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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