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, 2.5 m
Radar Cross Section
2.032 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 ONEWEB-0692
1 61600U 24188G 25260.91301302 .00000681 00000-0 18864-2 0 9994
2 61600 87.8767 75.3415 0001608 126.3835 233.7442 13.11433730 48784Epoch: 2025-09-17T21:54Z
TLE epoch observation values (Epoch: 2025-09-17T21:54:44.324Z)
Latitude
0.00001°
Longitude
109.57467°
Altitude
1,221.23 km
Speed
7.243 km/s
True Right ascension
05h 01m 21s
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
05:14:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,215.957 km
Perigee altitude
1,213.515 km
Semi-major axis
7,592.873 km
Eccentricity
0.00016
Inclination
87.8767°
RAAN
75.3415°
Arg. of periapsis
126.3835°
True anomaly
233.72934°
Mean anomaly
233.7442°
Eccentric anomaly
233.73677°
Mean motion
3.28045 °/min
Orbital period
109.74 mins
BSTAR
0.0018864
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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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2025-09-18 12:38:41.370Z | 195.209° SSW | 2025-09-18 12:45:41.370Z | 267.575° W | 40.526° | 2025-09-18 12:52:41.370Z | 352.238° N |
| 8 mins | 2025-09-18 22:21:41.370Z | 43.173° NE | 2025-09-18 22:24:41.370Z | 71.73° E | 18.414° | 2025-09-18 22:29:41.370Z | 116.444° SE |
| 13 mins | 2025-09-19 00:09:41.370Z | 353.973° N | 2025-09-19 00:15:41.370Z | 262.495° W | 43.712° | 2025-09-19 00:22:41.370Z | 190.158° SSW |
| 9 mins | 2025-09-19 10:40:41.370Z | 114.964° SE | 2025-09-19 10:44:41.370Z | 77.492° E | 20.492° | 2025-09-19 10:49:41.370Z | 31.42° NE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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