ONEWEB-0693, 61601
Orbit data source: Space-Track
ONEWEB-0693, 61601 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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61601 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 ONEWEB-0693
1 61601U 24188H 25256.18019220 .00000012 00000-0 -21497-5 0 9992
2 61601 87.9034 61.0290 0001575 62.6442 297.4850 13.17647557 49405Epoch: 2025-09-13T04:19Z
TLE epoch observation values (Epoch: 2025-09-13T04:19:28.606Z)
Latitude
0.00003°
Longitude
3.74256°
Altitude
1,196.067 km
Speed
7.256 km/s
True Right ascension
04h 04m 06s
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
18:51:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,192.02 km
Perigee altitude
1,189.636 km
Semi-major axis
7,568.965 km
Eccentricity
0.00016
Inclination
87.9034°
RAAN
61.029°
Arg. of periapsis
62.6442°
True anomaly
297.46899°
Mean anomaly
297.485°
Eccentric anomaly
297.47699°
Mean motion
3.29601 °/min
Orbital period
109.22 mins
BSTAR
-0.0000021497
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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-0693 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 | 2025-09-14 09:39:48.697Z | 91.727° ESE | 2025-09-14 09:42:48.697Z | 65.895° ENE | 12.893° | 2025-09-14 09:44:48.697Z | 48.994° ENE |
| 12 mins | 2025-09-14 11:24:48.697Z | 174.77° S | 2025-09-14 11:30:48.697Z | 43.067° NE | 44.638° | 2025-09-14 11:36:48.697Z | 2.364° NNE |
| 7 mins | 2025-09-14 13:17:48.697Z | 260.383° W | 2025-09-14 13:20:48.697Z | 287.848° WNW | 15.667° | 2025-09-14 13:24:48.697Z | 322.534° NNW |
| 13 mins | 2025-09-14 22:50:48.697Z | 7.473° NNE | 2025-09-14 22:56:48.697Z | 80.826° E | 41.937° | 2025-09-14 23:03:48.697Z | 167.629° S |
| 9 mins | 2025-09-15 00:41:48.697Z | 322.776° NNW | 2025-09-15 00:45:48.697Z | 282.979° WNW | 20.723° | 2025-09-15 00:50:48.697Z | 238.193° WSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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