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: 9 hours ago
TLE from 9 hours ago
0 ONEWEB-0692
1 61600U 24188G 26133.73005951 -.00000640 00000-0 -18419-2 0 9998
2 61600 87.8921 27.9376 0001044 67.8321 292.2918 13.11415264 79951Epoch: 2026-05-13T17:31Z
TLE epoch observation values (Epoch: 2026-05-13T17:31:17.141Z)
Latitude
0°
Longitude
-106.36971°
Altitude
1,220.278 km
Speed
7.244 km/s
True Right ascension
01h 51m 45s
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
11:22:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,215.6 km
Perigee altitude
1,214.015 km
Semi-major axis
7,592.944 km
Eccentricity
0.0001
Inclination
87.8921°
RAAN
27.9376°
Arg. of periapsis
67.8321°
True anomaly
292.28073°
Mean anomaly
292.2918°
Eccentric anomaly
292.28627°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
-0.0018419
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-14 03:18:51.160Z | 42.864° NE | 2026-05-14 03:21:51.160Z | 67.684° E | 13.486° | 2026-05-14 03:24:51.160Z | 93.512° ESE |
| 13 mins | 2026-05-14 05:06:51.160Z | 0.743° NNE | 2026-05-14 05:12:51.160Z | 32.795° NE | 44.706° | 2026-05-14 05:19:51.160Z | 179.135° S |
| 6 mins | 2026-05-14 06:59:51.160Z | 308.299° NW | 2026-05-14 07:01:51.160Z | 290.048° WNW | 15.552° | 2026-05-14 07:05:51.160Z | 255.575° W |
| 7 mins | 2026-05-14 15:39:51.160Z | 98.435° ESE | 2026-05-14 15:42:51.160Z | 71.908° E | 15.399° | 2026-05-14 15:46:51.160Z | 38.113° NE |
| 13 mins | 2026-05-14 17:25:51.160Z | 180.795° SSW | 2026-05-14 17:31:51.160Z | 306.043° NW | 44.906° | 2026-05-14 17:38:51.160Z | 359.827° N |
| 5 mins | 2026-05-14 19:20:51.160Z | 272.874° WNW | 2026-05-14 19:22:51.160Z | 290.492° WNW | 13.668° | 2026-05-14 19:25:51.160Z | 315.714° NNW |
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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