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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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 26305.41668980 .00006626 00000-0 18648-1 0 9992
2 61600 87.8925 353.8174 0002149 120.5316 328.6677 13.11407076 5238Epoch: 2026-11-01T10:00Z
TLE epoch observation values (Epoch: 2026-11-01T10:00:01.998Z)
Latitude
87.75203°
Longitude
-128.03602°
Altitude
1,230.202 km
Speed
7.247 km/s
True Right ascension
04h 10m 43s
True Declination
87° 44' 22"
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
00:23:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.471 km
Perigee altitude
1,213.207 km
Semi-major axis
7,592.976 km
Eccentricity
0.00021
Inclination
87.8925°
RAAN
353.8174°
Arg. of periapsis
120.5316°
True anomaly
328.65489°
Mean anomaly
328.6677°
Eccentric anomaly
328.6613°
Mean motion
3.28039 °/min
Orbital period
109.74 mins
BSTAR
0.018648
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-02 05:52:29.844Z | 271.034° WNW | 2026-11-02 05:54:29.844Z | 287.853° WNW | 13.001° | 2026-11-02 05:57:29.844Z | 312.811° NW |
| 5 mins | 2026-11-02 13:40:29.844Z | 54.012° ENE | 2026-11-02 13:42:29.844Z | 71.086° E | 13.185° | 2026-11-02 13:45:29.844Z | 95.862° ESE |
| 13 mins | 2026-11-02 15:27:29.844Z | 2.058° NNE | 2026-11-02 15:33:29.844Z | 95.981° ESE | 82.107° | 2026-11-02 15:40:29.844Z | 177.54° S |
| 7 mins | 2026-11-02 17:19:29.844Z | 313.809° NW | 2026-11-02 17:22:29.844Z | 286.359° WNW | 17.093° | 2026-11-02 17:26:29.844Z | 252.159° W |
| 6 mins | 2026-11-03 02:00:29.844Z | 94.433° ESE | 2026-11-03 02:03:29.844Z | 67.933° E | 15.165° | 2026-11-03 02:06:29.844Z | 42.637° NE |
| 12 mins | 2026-11-03 03:46:29.844Z | 178.811° S | 2026-11-03 03:51:29.844Z | 181.391° SSW | 81.21° | 2026-11-03 03:58:29.844Z | 0.502° NNE |
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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