ONEWEB-0603, 54667
Orbit data source: Space-Track
ONEWEB-0603, 54667 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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54667 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-0603
1 54667U 22166AB 26171.18431299 .00000060 00000-0 11446-3 0 9994
2 54667 87.9260 243.3619 0001957 96.0482 264.0875 13.21826655171876Epoch: 2026-06-20T04:25Z
TLE epoch observation values (Epoch: 2026-06-20T04:25:24.642Z)
Latitude
-0.00001°
Longitude
-91.39335°
Altitude
1,180.808 km
Speed
7.263 km/s
True Right ascension
16h 13m 26s
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
00:51:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,176.332 km
Perigee altitude
1,173.375 km
Semi-major axis
7,552.99 km
Eccentricity
0.0002
Inclination
87.926°
RAAN
243.3619°
Arg. of periapsis
96.0482°
True anomaly
264.06519°
Mean anomaly
264.0875°
Eccentric anomaly
264.07635°
Mean motion
3.30647 °/min
Orbital period
108.88 mins
BSTAR
0.00011446
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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-0603 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 15:11:54.756Z | 45.296° ENE | 2026-06-22 15:14:54.756Z | 72.358° E | 15.024° | 2026-06-22 15:17:54.756Z | 99.514° ESE |
| 13 mins | 2026-06-22 16:58:54.756Z | 358.243° N | 2026-06-22 17:04:54.756Z | 255.923° W | 44.915° | 2026-06-22 17:11:54.756Z | 183.675° SSW |
| 5 mins | 2026-06-22 18:50:54.756Z | 305.541° NW | 2026-06-22 18:52:54.756Z | 287.731° WNW | 13.279° | 2026-06-22 18:55:54.756Z | 262.35° W |
| 6 mins | 2026-06-23 03:26:54.756Z | 96.437° ESE | 2026-06-23 03:29:54.756Z | 68.566° E | 15.389° | 2026-06-23 03:32:54.756Z | 42.128° NE |
| 12 mins | 2026-06-23 05:11:54.756Z | 182.009° SSW | 2026-06-23 05:17:54.756Z | 320.598° NNW | 44.639° | 2026-06-23 05:23:54.756Z | 358.915° N |
| 4 mins | 2026-06-23 07:05:54.756Z | 273.458° WNW | 2026-06-23 07:07:54.756Z | 291.144° WNW | 12.864° | 2026-06-23 07:09:54.756Z | 308.501° 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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