ONEWEB-0664, 55824
Orbit data source: Space-Track
ONEWEB-0664, 55824 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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55824 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: 10 hours ago
TLE from 10 hours ago
0 ONEWEB-0664
1 55824U 23029AE 26112.28295879 .00000118 00000-0 25870-3 0 9997
2 55824 87.9127 285.6463 0002204 101.1200 259.0181 13.20769121153767Epoch: 2026-04-22T06:47Z
TLE epoch observation values (Epoch: 2026-04-22T06:47:27.639Z)
Latitude
-0.00004°
Longitude
-26.56548°
Altitude
1,185.005 km
Speed
7.261 km/s
True Right ascension
19h 02m 35s
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
23:35:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,180.553 km
Perigee altitude
1,177.222 km
Semi-major axis
7,557.025 km
Eccentricity
0.00022
Inclination
87.9127°
RAAN
285.6463°
Arg. of periapsis
101.12°
True anomaly
258.99331°
Mean anomaly
259.0181°
Eccentric anomaly
259.0057°
Mean motion
3.30382 °/min
Orbital period
108.96 mins
BSTAR
0.0002587
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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-0664 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-04-22 21:57:54.440Z | 40.4° NE | 2026-04-22 22:01:54.440Z | 74.977° E | 14.194° | 2026-04-22 22:04:54.440Z | 100.9° ESE |
| 12 mins | 2026-04-22 23:45:54.440Z | 359.437° N | 2026-04-22 23:51:54.440Z | 185.298° SSW | 44.883° | 2026-04-22 23:57:54.440Z | 181.705° SSW |
| 5 mins | 2026-04-23 01:37:54.440Z | 304.97° NW | 2026-04-23 01:39:54.440Z | 286.713° WNW | 14.112° | 2026-04-23 01:42:54.440Z | 260.892° W |
| 5 mins | 2026-04-23 10:14:54.440Z | 90.06° ESE | 2026-04-23 10:16:54.440Z | 71.592° E | 14.781° | 2026-04-23 10:19:54.440Z | 44.965° NE |
| 13 mins | 2026-04-23 11:58:54.440Z | 179.994° S | 2026-04-23 12:04:54.440Z | 242.816° WSW | 44.963° | 2026-04-23 12:11:54.440Z | 0.052° NNE |
| 5 mins | 2026-04-23 13:52:54.440Z | 269.029° W | 2026-04-23 13:54:54.440Z | 286.756° WNW | 13.584° | 2026-04-23 13:57:54.440Z | 312.994° NW |
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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