ONEWEB-0695, 61602
Orbit data source: Space-Track
ONEWEB-0695, 61602 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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61602 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 ONEWEB-0695
1 61602U 24188J 25310.02441638 .00000185 00000-0 48735-3 0 9991
2 61602 87.8850 65.5240 0001860 84.2390 275.8950 13.11416521 55210Epoch: 2025-11-06T00:35Z
TLE epoch observation values (Epoch: 2025-11-06T00:35:09.575Z)
Latitude
-0°
Longitude
11.24543°
Altitude
1,220.429 km
Speed
7.244 km/s
True Right ascension
04h 22m 05s
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
16:30:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.215 km
Perigee altitude
1,213.39 km
Semi-major axis
7,592.94 km
Eccentricity
0.00019
Inclination
87.885°
RAAN
65.524°
Arg. of periapsis
84.239°
True anomaly
275.8738°
Mean anomaly
275.895°
Eccentric anomaly
275.8844°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
0.00048735
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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-0695 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-11-06 21:20:23.506Z | 334.453° NNW | 2025-11-06 21:25:23.506Z | 289.167° WNW | 24.173° | 2025-11-06 21:31:23.506Z | 231.241° WSW |
| 12 mins | 2025-11-07 07:49:23.506Z | 159.888° S | 2025-11-07 07:55:23.506Z | 75.666° E | 40.952° | 2025-11-07 08:01:23.506Z | 9.541° NNE |
| 9 mins | 2025-11-07 09:41:23.506Z | 242.154° WSW | 2025-11-07 09:45:23.506Z | 282.276° WNW | 22.076° | 2025-11-07 09:50:23.506Z | 330.188° NNW |
| 12 mins | 2025-11-07 19:19:23.506Z | 16.517° NNE | 2025-11-07 19:24:23.506Z | 76.765° E | 36.688° | 2025-11-07 19:31:23.506Z | 156.473° SSE |
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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