ONEWEB-0652, 55814
Orbit data source: Space-Track
ONEWEB-0652, 55814 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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55814 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-0652
1 55814U 23029U 26171.36640060 -.00005733 00000-0 -15502-1 0 9995
2 55814 87.8966 289.0769 0001966 103.5045 256.6304 13.14530403159780Epoch: 2026-06-20T08:47Z
TLE epoch observation values (Epoch: 2026-06-20T08:47:37.011Z)
Latitude
-0.00003°
Longitude
-111.40937°
Altitude
1,208.923 km
Speed
7.249 km/s
True Right ascension
19h 16m 18s
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
21:43:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,204.288 km
Perigee altitude
1,201.307 km
Semi-major axis
7,580.935 km
Eccentricity
0.0002
Inclination
87.8966°
RAAN
289.0769°
Arg. of periapsis
103.5045°
True anomaly
256.60848°
Mean anomaly
256.6304°
Eccentric anomaly
256.61944°
Mean motion
3.28821 °/min
Orbital period
109.48 mins
BSTAR
-0.015502
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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-0652 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 18:04:28.776Z | 49.758° ENE | 2026-06-22 18:06:28.776Z | 66.608° ENE | 12.753° | 2026-06-22 18:09:28.776Z | 92.191° ESE |
| 13 mins | 2026-06-22 19:51:28.776Z | 1.633° NNE | 2026-06-22 19:57:28.776Z | 59.543° ENE | 44.691° | 2026-06-22 20:04:28.776Z | 177.735° S |
| 7 mins | 2026-06-22 21:43:28.776Z | 313.797° NW | 2026-06-22 21:46:28.776Z | 286.304° WNW | 16.063° | 2026-06-22 21:50:28.776Z | 252.114° W |
| 6 mins | 2026-06-23 06:23:28.776Z | 92.934° ESE | 2026-06-23 06:25:28.776Z | 75.528° E | 14.138° | 2026-06-23 06:29:28.776Z | 41.43° NE |
| 13 mins | 2026-06-23 08:08:28.776Z | 177.938° S | 2026-06-23 08:14:28.776Z | 97.018° ESE | 44.995° | 2026-06-23 08:21:28.776Z | 0.95° NNE |
| 6 mins | 2026-06-23 10:02:28.776Z | 264.804° W | 2026-06-23 10:05:28.776Z | 291.681° WNW | 14.557° | 2026-06-23 10:08:28.776Z | 317.365° 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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