ONEWEB-0655, 54677
Orbit data source: Space-Track
ONEWEB-0655, 54677 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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54677 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-0655
1 54677U 22166AM 26171.48204844 .00000116 00000-0 24844-3 0 9990
2 54677 87.9253 243.3330 0001782 95.6462 264.4875 13.21827641171878Epoch: 2026-06-20T11:34Z
TLE epoch observation values (Epoch: 2026-06-20T11:34:08.985Z)
Latitude
-0.00002°
Longitude
161.09952°
Altitude
1,180.781 km
Speed
7.263 km/s
True Right ascension
16h 13m 19s
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
23:18:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,176.196 km
Perigee altitude
1,173.504 km
Semi-major axis
7,552.987 km
Eccentricity
0.00018
Inclination
87.9253°
RAAN
243.333°
Arg. of periapsis
95.6462°
True anomaly
264.46717°
Mean anomaly
264.4875°
Eccentric anomaly
264.47734°
Mean motion
3.30647 °/min
Orbital period
108.88 mins
BSTAR
0.00024844
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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-0655 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 15:04:33.145Z | 45.802° ENE | 2026-06-22 15:07:33.145Z | 71.526° E | 13.081° | 2026-06-22 15:10:33.145Z | 97.155° ESE |
| 13 mins | 2026-06-22 16:51:33.145Z | 0.989° NNE | 2026-06-22 16:57:33.145Z | 81.038° E | 44.894° | 2026-06-22 17:04:33.145Z | 179.148° S |
| 5 mins | 2026-06-22 18:43:33.145Z | 307.232° NW | 2026-06-22 18:45:33.145Z | 288.534° WNW | 15.237° | 2026-06-22 18:48:33.145Z | 261.344° W |
| 5 mins | 2026-06-23 03:20:33.145Z | 87.452° E | 2026-06-23 03:22:33.145Z | 69.545° E | 13.478° | 2026-06-23 03:25:33.145Z | 44.014° NE |
| 12 mins | 2026-06-23 05:04:33.145Z | 176.635° S | 2026-06-23 05:10:33.145Z | 31.618° NE | 44.836° | 2026-06-23 05:16:33.145Z | 1.457° NNE |
| 6 mins | 2026-06-23 06:57:33.145Z | 263.076° W | 2026-06-23 07:00:33.145Z | 290.494° WNW | 14.785° | 2026-06-23 07:03:33.145Z | 316.899° 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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