ONEWEB-0649, 55812
Orbit data source: Space-Track
ONEWEB-0649, 55812 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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55812 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-0649
1 55812U 23029S 26171.34257889 .00000066 00000-0 13176-3 0 9993
2 55812 87.9174 304.3443 0001634 103.8999 256.2315 13.19725043159344Epoch: 2026-06-20T08:13Z
TLE epoch observation values (Epoch: 2026-06-20T08:13:18.816Z)
Latitude
-0.00006°
Longitude
-87.54268°
Altitude
1,188.966 km
Speed
7.259 km/s
True Right ascension
20h 17m 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
23:20:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,184.112 km
Perigee altitude
1,181.641 km
Semi-major axis
7,561.013 km
Eccentricity
0.00016
Inclination
87.9174°
RAAN
304.3443°
Arg. of periapsis
103.8999°
True anomaly
256.21331°
Mean anomaly
256.2315°
Eccentric anomaly
256.22241°
Mean motion
3.30121 °/min
Orbital period
109.05 mins
BSTAR
0.00013176
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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-0649 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 19:05:49.015Z | 49.838° ENE | 2026-06-22 19:07:49.015Z | 66.808° ENE | 12.554° | 2026-06-22 19:10:49.015Z | 92.542° ESE |
| 12 mins | 2026-06-22 20:52:49.015Z | 2.02° NNE | 2026-06-22 20:58:49.015Z | 125.708° SE | 44.631° | 2026-06-22 21:04:49.015Z | 177.403° S |
| 7 mins | 2026-06-22 22:43:49.015Z | 314.825° NW | 2026-06-22 22:46:49.015Z | 287.346° WNW | 15.897° | 2026-06-22 22:50:49.015Z | 252.589° W |
| 4 mins | 2026-06-23 07:22:49.015Z | 84.713° E | 2026-06-23 07:24:49.015Z | 66.846° ENE | 13.241° | 2026-06-23 07:26:49.015Z | 49.628° ENE |
| 12 mins | 2026-06-23 09:06:49.015Z | 175.865° S | 2026-06-23 09:12:49.015Z | 29.058° NE | 44.647° | 2026-06-23 09:18:49.015Z | 1.808° NNE |
| 6 mins | 2026-06-23 10:59:49.015Z | 262.542° W | 2026-06-23 11:02:49.015Z | 290.061° WNW | 15.148° | 2026-06-23 11:05:49.015Z | 316.649° 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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