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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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: 12 hours ago
TLE from 12 hours ago
0 ONEWEB-0695
1 61602U 24188J 26058.24885100 .00000537 00000-0 14794-2 0 9999
2 61602 87.8841 42.9424 0002403 85.7995 274.3408 13.11416731 70058Epoch: 2026-02-27T05:58Z
TLE epoch observation values (Epoch: 2026-02-27T05:58:20.726Z)
Latitude
0.00003°
Longitude
156.268°
Altitude
1,220.435 km
Speed
7.244 km/s
True Right ascension
02h 51m 46s
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
21:12:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.626 km
Perigee altitude
1,212.977 km
Semi-major axis
7,592.939 km
Eccentricity
0.00024
Inclination
87.8841°
RAAN
42.9424°
Arg. of periapsis
85.7995°
True anomaly
274.31334°
Mean anomaly
274.3408°
Eccentric anomaly
274.32707°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
0.0014794
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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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2026-02-27 22:32:47.820Z | 149.217° SSE | 2026-02-27 22:39:47.820Z | 76.137° E | 33.981° | 2026-02-27 22:45:47.820Z | 15.816° NNE |
| 11 mins | 2026-02-28 00:24:47.820Z | 225.972° WSW | 2026-02-28 00:29:47.820Z | 284.922° WNW | 29.238° | 2026-02-28 00:35:47.820Z | 342.046° N |
| 11 mins | 2026-02-28 10:03:47.820Z | 25.064° NE | 2026-02-28 10:08:47.820Z | 81.034° E | 29.215° | 2026-02-28 10:14:47.820Z | 141.256° SSE |
| 11 mins | 2026-02-28 11:53:47.820Z | 338.629° N | 2026-02-28 11:58:47.820Z | 276.247° WNW | 34.168° | 2026-02-28 12:04:47.820Z | 212.695° SW |
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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