ONEWEB-0534, 55797
Orbit data source: Space-Track
ONEWEB-0534, 55797 is a payload satellite owned by One Web (NAA) (UK) in LEO that was launched on Thu, 09 Mar 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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55797 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-0534
1 55797U 23029B 26171.33568596 .00000068 00000-0 13644-3 0 9996
2 55797 87.9187 273.8419 0001871 100.5906 259.5438 13.20771763161569Epoch: 2026-06-20T08:03Z
TLE epoch observation values (Epoch: 2026-06-20T08:03:23.266Z)
Latitude
-0.00006°
Longitude
-115.55682°
Altitude
1,184.934 km
Speed
7.261 km/s
True Right ascension
18h 15m 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
21:38:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,180.292 km
Perigee altitude
1,177.464 km
Semi-major axis
7,557.015 km
Eccentricity
0.00019
Inclination
87.9187°
RAAN
273.8419°
Arg. of periapsis
100.5906°
True anomaly
259.52272°
Mean anomaly
259.5438°
Eccentric anomaly
259.53326°
Mean motion
3.30383 °/min
Orbital period
108.96 mins
BSTAR
0.00013644
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Other satellites on launch #29 in the year 2023 (2023-03-09 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-0534 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 17:03:54.480Z | 49.116° ENE | 2026-06-22 17:06:54.480Z | 74.848° E | 12.434° | 2026-06-22 17:08:54.480Z | 91.791° ESE |
| 12 mins | 2026-06-22 18:50:54.480Z | 2.128° NNE | 2026-06-22 18:56:54.480Z | 123.909° SE | 44.61° | 2026-06-22 19:02:54.480Z | 177.206° S |
| 7 mins | 2026-06-22 20:41:54.480Z | 314.268° NW | 2026-06-22 20:44:54.480Z | 286.547° WNW | 15.934° | 2026-06-22 20:48:54.480Z | 251.905° W |
| 4 mins | 2026-06-23 05:20:54.480Z | 80.396° E | 2026-06-23 05:21:54.480Z | 71.468° E | 13.038° | 2026-06-23 05:24:54.480Z | 45.914° ENE |
| 13 mins | 2026-06-23 07:03:54.480Z | 175.386° S | 2026-06-23 07:09:54.480Z | 100.284° ESE | 44.857° | 2026-06-23 07:16:54.480Z | 2.013° NNE |
| 7 mins | 2026-06-23 08:56:54.480Z | 259.565° W | 2026-06-23 08:59:54.480Z | 286.801° WNW | 15.369° | 2026-06-23 09:03:54.480Z | 321.755° 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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