ONEWEB-0616, 55157
Orbit data source: Space-Track
ONEWEB-0616, 55157 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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55157 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: 3 days ago
TLE from 3 days ago
0 ONEWEB-0616
1 55157U 23004T 26170.95267418 .00000040 00000-0 69661-4 0 9996
2 55157 87.9133 5.3173 0000940 85.3550 274.7689 13.17649303168065Epoch: 2026-06-19T22:51Z
TLE epoch observation values (Epoch: 2026-06-19T22:51:51.049Z)
Latitude
0.00001°
Longitude
114.18033°
Altitude
1,196.551 km
Speed
7.256 km/s
True Right ascension
00h 21m 16s
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
00:27:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,191.532 km
Perigee altitude
1,190.109 km
Semi-major axis
7,568.958 km
Eccentricity
0.00009
Inclination
87.9133°
RAAN
5.3173°
Arg. of periapsis
85.355°
True anomaly
274.75817°
Mean anomaly
274.7689°
Eccentric anomaly
274.76353°
Mean motion
3.29601 °/min
Orbital period
109.22 mins
BSTAR
0.000069661
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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-0616 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-06-22 14:47:13.162Z | 240.934° WSW | 2026-06-22 14:52:13.162Z | 289.511° WNW | 20.385° | 2026-06-22 14:56:13.162Z | 326.894° NNW |
| 12 mins | 2026-06-23 00:22:13.162Z | 13.523° NNE | 2026-06-23 00:28:13.162Z | 85.506° E | 36.923° | 2026-06-23 00:34:13.162Z | 155.141° SSE |
| 10 mins | 2026-06-23 02:12:13.162Z | 333.036° NNW | 2026-06-23 02:17:13.162Z | 281.347° WNW | 26.122° | 2026-06-23 02:22:13.162Z | 230.315° WSW |
| 12 mins | 2026-06-23 12:38:13.162Z | 151.911° SSE | 2026-06-23 12:43:13.162Z | 89.583° E | 38.039° | 2026-06-23 12:50:13.162Z | 10.997° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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