ONEWEB-0688, 61596
Orbit data source: Space-Track
ONEWEB-0688, 61596 is a payload satellite owned by Eut. One Web (UK) in LEO that was launched on Sun, 20 Oct 2024 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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61596 intel report (Beta)
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Edit Public Description
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: 8 hours ago
TLE from 8 hours ago
0 ONEWEB-0688
1 61596U 24188C 25336.73665620 .00000207 00000-0 50062-3 0 9999
2 61596 87.9112 44.9639 0001951 142.5086 217.6182 13.17650403 60029Epoch: 2025-12-02T17:40Z
TLE epoch observation values (Epoch: 2025-12-02T17:40:47.095Z)
Latitude
-0.00002°
Longitude
67.95015°
Altitude
1,197.777 km
Speed
7.254 km/s
True Right ascension
02h 59m 51s
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
23:05:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,192.293 km
Perigee altitude
1,189.34 km
Semi-major axis
7,568.954 km
Eccentricity
0.0002
Inclination
87.9112°
RAAN
44.9639°
Arg. of periapsis
142.5086°
True anomaly
217.60456°
Mean anomaly
217.6182°
Eccentric anomaly
217.61138°
Mean motion
3.29602 °/min
Orbital period
109.22 mins
BSTAR
0.00050062
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Other satellites on launch #188 in the year 2024 (2024-10-20 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-0688 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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2025-12-03 04:42:17.979Z | 160.637° S | 2025-12-03 04:49:17.979Z | 76.666° E | 40.162° | 2025-12-03 04:55:17.979Z | 10.265° NNE |
| 10 mins | 2025-12-03 06:34:17.979Z | 237.372° WSW | 2025-12-03 06:39:17.979Z | 288.588° WNW | 22.543° | 2025-12-03 06:44:17.979Z | 334.126° NNW |
| 11 mins | 2025-12-03 16:10:17.979Z | 19.828° NNE | 2025-12-03 16:15:17.979Z | 82.823° E | 34.54° | 2025-12-03 16:21:17.979Z | 150.62° SSE |
| 11 mins | 2025-12-03 17:59:17.979Z | 335.639° NNW | 2025-12-03 18:04:17.979Z | 283.094° WNW | 28.443° | 2025-12-03 18:10:17.979Z | 222.415° SW |
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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