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, 2.5 m
Radar Cross Section
2.032 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 ONEWEB-0695
1 61602U 24188J 25256.23518152 -.00000282 00000-0 -83161-3 0 9991
2 61602 87.8772 76.2637 0001812 107.9577 252.1749 13.11417652 48165Epoch: 2025-09-13T05:38Z
TLE epoch observation values (Epoch: 2025-09-13T05:38:39.683Z)
Latitude
0.00003°
Longitude
-0.8731°
Altitude
1,220.991 km
Speed
7.244 km/s
True Right ascension
05h 05m 03s
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
18:51:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.174 km
Perigee altitude
1,213.422 km
Semi-major axis
7,592.935 km
Eccentricity
0.00018
Inclination
87.8772°
RAAN
76.2637°
Arg. of periapsis
107.9577°
True anomaly
252.15513°
Mean anomaly
252.1749°
Eccentric anomaly
252.16502°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
-0.00083161
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-09-14 11:05:49.609Z | 110.521° ESE | 2025-09-14 11:09:49.609Z | 70.062° E | 20.687° | 2025-09-14 11:13:49.609Z | 33.385° NE |
| 13 mins | 2025-09-14 12:52:49.609Z | 194.327° SSW | 2025-09-14 12:58:49.609Z | 283.376° WNW | 42.09° | 2025-09-14 13:05:49.609Z | 354.741° N |
| 7 mins | 2025-09-14 22:34:49.609Z | 47.57° ENE | 2025-09-14 22:37:49.609Z | 75.722° E | 16.683° | 2025-09-14 22:41:49.609Z | 110.347° ESE |
| 12 mins | 2025-09-15 00:22:49.609Z | 356.065° N | 2025-09-15 00:27:49.609Z | 316.167° NNW | 44.192° | 2025-09-15 00:34:49.609Z | 186.816° SSW |
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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