ONEWEB-0681, 56717
Orbit data source: Space-Track
ONEWEB-0681, 56717 is a payload satellite owned by One Web (NAA) (UK) in LEO that was launched on Sat, 20 May 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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56717 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-0681
1 56717U 23068H 26171.48287505 -.00000033 00000-0 -11064-3 0 9994
2 56717 87.9255 243.3166 0001813 70.0939 290.0390 13.21827452151522Epoch: 2026-06-20T11:35Z
TLE epoch observation values (Epoch: 2026-06-20T11:35:20.404Z)
Latitude
-0.00003°
Longitude
160.78473°
Altitude
1,180.183 km
Speed
7.264 km/s
True Right ascension
16h 13m 15s
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
21:32:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,176.22 km
Perigee altitude
1,173.481 km
Semi-major axis
7,552.987 km
Eccentricity
0.00018
Inclination
87.9255°
RAAN
243.3166°
Arg. of periapsis
70.0939°
True anomaly
290.01948°
Mean anomaly
290.039°
Eccentric anomaly
290.02924°
Mean motion
3.30647 °/min
Orbital period
108.88 mins
BSTAR
-0.00011064
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Other satellites on launch #68 in the year 2023 (2023-05-20 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-0681 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-22 15:05:36.262Z | 44.553° NE | 2026-06-22 15:08:36.262Z | 70.266° E | 13.406° | 2026-06-22 15:11:36.262Z | 96.351° ESE |
| 13 mins | 2026-06-22 16:52:36.262Z | 0.462° NNE | 2026-06-22 16:58:36.262Z | 42.125° NE | 44.893° | 2026-06-22 17:05:36.262Z | 179.877° S |
| 5 mins | 2026-06-22 18:44:36.262Z | 308.244° NW | 2026-06-22 18:46:36.262Z | 289.854° WNW | 14.897° | 2026-06-22 18:49:36.262Z | 262.729° W |
| 5 mins | 2026-06-23 03:21:36.262Z | 88.807° E | 2026-06-23 03:23:36.262Z | 70.806° E | 13.806° | 2026-06-23 03:26:36.262Z | 44.85° NE |
| 13 mins | 2026-06-23 05:05:36.262Z | 177.541° S | 2026-06-23 05:11:36.262Z | 37.009° NE | 44.964° | 2026-06-23 05:18:36.262Z | 1.101° NNE |
| 5 mins | 2026-06-23 06:59:36.262Z | 270.648° WNW | 2026-06-23 07:01:36.262Z | 289.161° WNW | 14.471° | 2026-06-23 07:04:36.262Z | 315.62° 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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