ONEWEB-0628, 55169
Orbit data source: Space-Track
ONEWEB-0628, 55169 is a payload satellite owned by One Web (NAA) (UK) in LEO that was launched on Tue, 10 Jan 2023 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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55169 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-0628
1 55169U 23004AF 26171.45450331 -.00000496 00000-0 -14143-2 0 9993
2 55169 87.8944 350.0031 0002222 76.4953 283.6423 13.12443016168460Epoch: 2026-06-20T10:54Z
TLE epoch observation values (Epoch: 2026-06-20T10:54:29.085Z)
Latitude
-0.00005°
Longitude
-82.28698°
Altitude
1,216.216 km
Speed
7.246 km/s
True Right ascension
23h 20m 00s
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
00:39:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,212.526 km
Perigee altitude
1,209.154 km
Semi-major axis
7,588.977 km
Eccentricity
0.00022
Inclination
87.8944°
RAAN
350.0031°
Arg. of periapsis
76.4953°
True anomaly
283.61755°
Mean anomaly
283.6423°
Eccentric anomaly
283.62993°
Mean motion
3.28298 °/min
Orbital period
109.66 mins
BSTAR
-0.0014143
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Other satellites on launch #4 in the year 2023 (2023-01-10 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-0628 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-22 14:19:10.835Z | 268.697° W | 2026-06-22 14:22:10.835Z | 293.942° NW | 12.41° | 2026-06-22 14:24:10.835Z | 310.533° NW |
| 4 mins | 2026-06-22 22:07:10.835Z | 54.913° ENE | 2026-06-22 22:09:10.835Z | 72.068° E | 12.71° | 2026-06-22 22:11:10.835Z | 89.008° E |
| 13 mins | 2026-06-22 23:54:10.835Z | 2.287° NNE | 2026-06-23 00:00:10.835Z | 121.047° SE | 44.607° | 2026-06-23 00:07:10.835Z | 177.546° S |
| 6 mins | 2026-06-23 01:46:10.835Z | 311.596° NW | 2026-06-23 01:49:10.835Z | 283.585° WNW | 16.282° | 2026-06-23 01:52:10.835Z | 257.122° W |
| 5 mins | 2026-06-23 10:27:10.835Z | 89.148° E | 2026-06-23 10:29:10.835Z | 71.278° E | 14.399° | 2026-06-23 10:32:10.835Z | 45.375° ENE |
| 13 mins | 2026-06-23 12:12:10.835Z | 178.249° S | 2026-06-23 12:18:10.835Z | 4.774° NNE | 44.85° | 2026-06-23 12:25:10.835Z | 0.878° NNE |
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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