ONEWEB-0679, 56715
Orbit data source: Space-Track
ONEWEB-0679, 56715 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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56715 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-0679
1 56715U 23068F 26171.20754606 .00000476 00000-0 12113-2 0 9997
2 56715 87.9086 228.1703 0002612 88.9147 271.2283 13.16598222152120Epoch: 2026-06-20T04:58Z
TLE epoch observation values (Epoch: 2026-06-20T04:58:51.979Z)
Latitude
-0.00004°
Longitude
-114.97176°
Altitude
1,200.596 km
Speed
7.254 km/s
True Right ascension
15h 12m 40s
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
21:29:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,196.83 km
Perigee altitude
1,192.874 km
Semi-major axis
7,572.989 km
Eccentricity
0.00026
Inclination
87.9086°
RAAN
228.1703°
Arg. of periapsis
88.9147°
True anomaly
271.19838°
Mean anomaly
271.2283°
Eccentric anomaly
271.21334°
Mean motion
3.29338 °/min
Orbital period
109.31 mins
BSTAR
0.0012113
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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-0679 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 | 2026-06-22 14:09:49.843Z | 44.831° NE | 2026-06-22 14:12:49.843Z | 71.406° E | 14.958° | 2026-06-22 14:16:49.843Z | 105.829° ESE |
| 12 mins | 2026-06-22 15:57:49.843Z | 358.555° N | 2026-06-22 16:02:49.843Z | 344.068° N | 44.525° | 2026-06-22 16:09:49.843Z | 183.144° SSW |
| 5 mins | 2026-06-22 17:49:49.843Z | 305.235° NW | 2026-06-22 17:51:49.843Z | 287.405° WNW | 13.709° | 2026-06-22 17:54:49.843Z | 262.065° W |
| 6 mins | 2026-06-23 02:27:49.843Z | 96.808° ESE | 2026-06-23 02:30:49.843Z | 68.701° E | 16.076° | 2026-06-23 02:33:49.843Z | 42.1° NE |
| 13 mins | 2026-06-23 04:12:49.843Z | 183.036° SSW | 2026-06-23 04:18:49.843Z | 253.891° W | 44.699° | 2026-06-23 04:25:49.843Z | 358.684° N |
| 4 mins | 2026-06-23 06:07:49.843Z | 274.792° WNW | 2026-06-23 06:09:49.843Z | 292.138° WNW | 12.571° | 2026-06-23 06:11:49.843Z | 309.095° 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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