ONEWEB-0648, 55811
Orbit data source: Space-Track
ONEWEB-0648, 55811 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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55811 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: 18 hours ago
TLE from 18 hours ago
0 ONEWEB-0648
1 55811U 23029R 26111.93746679 -.00000201 00000-0 -57647-3 0 9995
2 55811 87.8929 300.9301 0002523 76.1358 284.0052 13.14502004152002Epoch: 2026-04-21T22:29Z
TLE epoch observation values (Epoch: 2026-04-21T22:29:57.130Z)
Latitude
-0.00006°
Longitude
113.43598°
Altitude
1,208.224 km
Speed
7.25 km/s
True Right ascension
20h 03m 43s
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
23:41:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,204.82 km
Perigee altitude
1,200.994 km
Semi-major axis
7,581.044 km
Eccentricity
0.00025
Inclination
87.8929°
RAAN
300.9301°
Arg. of periapsis
76.1358°
True anomaly
283.97715°
Mean anomaly
284.0052°
Eccentric anomaly
283.99117°
Mean motion
3.28813 °/min
Orbital period
109.48 mins
BSTAR
-0.00057647
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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-0648 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 | 2026-04-22 22:53:55.106Z | 49.958° ENE | 2026-04-22 22:55:55.106Z | 66.968° ENE | 13.064° | 2026-04-22 22:58:55.106Z | 92.756° ESE |
| 13 mins | 2026-04-23 00:40:55.106Z | 1.231° NNE | 2026-04-23 00:46:55.106Z | 60.292° ENE | 44.803° | 2026-04-23 00:53:55.106Z | 178.503° S |
| 6 mins | 2026-04-23 02:32:55.106Z | 313.234° NW | 2026-04-23 02:35:55.106Z | 285.886° WNW | 15.732° | 2026-04-23 02:38:55.106Z | 259.283° W |
| 6 mins | 2026-04-23 11:12:55.106Z | 92.805° ESE | 2026-04-23 11:14:55.106Z | 75.17° E | 14.454° | 2026-04-23 11:18:55.106Z | 40.924° NE |
| 13 mins | 2026-04-23 12:57:55.106Z | 178.767° S | 2026-04-23 13:03:55.106Z | 334.827° NNW | 44.997° | 2026-04-23 13:10:55.106Z | 0.621° NNE |
| 6 mins | 2026-04-23 14:51:55.106Z | 265.393° W | 2026-04-23 14:54:55.106Z | 292.056° WNW | 14.232° | 2026-04-23 14:57:55.106Z | 317.504° 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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