ONEWEB-0692, 61600
Orbit data source: Space-Track
ONEWEB-0692, 61600 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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61600 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: 19 hours ago
TLE from 19 hours ago
0 ONEWEB-0692
1 61600U 24188G 25348.19654111 .00000523 00000-0 14410-2 0 9998
2 61600 87.8852 57.9312 0001182 72.2201 287.9056 13.11415421 60226Epoch: 2025-12-14T04:43Z
TLE epoch observation values (Epoch: 2025-12-14T04:43:01.151Z)
Latitude
-0.00003°
Longitude
-95.93652°
Altitude
1,220.302 km
Speed
7.244 km/s
True Right ascension
03h 51m 43s
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
22:19:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,215.704 km
Perigee altitude
1,213.909 km
Semi-major axis
7,592.944 km
Eccentricity
0.00012
Inclination
87.8852°
RAAN
57.9312°
Arg. of periapsis
72.2201°
True anomaly
287.89271°
Mean anomaly
287.9056°
Eccentric anomaly
287.89916°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
0.001441
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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-0692 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 | 2025-12-15 04:37:33.969Z | 152.767° SSE | 2025-12-15 04:43:33.969Z | 83.988° E | 37.36° | 2025-12-15 04:50:33.969Z | 11.392° NNE |
| 11 mins | 2025-12-15 06:28:33.969Z | 228.674° WSW | 2025-12-15 06:33:33.969Z | 279.185° WNW | 26.01° | 2025-12-15 06:39:33.969Z | 337.749° N |
| 12 mins | 2025-12-15 16:07:33.969Z | 19.802° NNE | 2025-12-15 16:12:33.969Z | 73.946° E | 32.436° | 2025-12-15 16:19:33.969Z | 148.952° SSE |
| 11 mins | 2025-12-15 17:57:33.969Z | 337.208° NNW | 2025-12-15 18:02:33.969Z | 283.195° WNW | 30.77° | 2025-12-15 18:08:33.969Z | 219.525° 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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