ONEWEB-0702, 61608
Orbit data source: Space-Track
ONEWEB-0702, 61608 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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61608 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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 ONEWEB-0702
1 61608U 24188Q 26035.56834572 .00000282 00000-0 75964-3 0 9996
2 61608 87.8827 47.3574 0002245 118.5570 241.5784 13.11415406 67104Epoch: 2026-02-04T13:38Z
TLE epoch observation values (Epoch: 2026-02-04T13:38:25.070Z)
Latitude
-0.00002°
Longitude
68.01988°
Altitude
1,221.39 km
Speed
7.243 km/s
True Right ascension
03h 09m 25s
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
06:07:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.512 km
Perigee altitude
1,213.102 km
Semi-major axis
7,592.944 km
Eccentricity
0.00022
Inclination
87.8827°
RAAN
47.3574°
Arg. of periapsis
118.557°
True anomaly
241.55578°
Mean anomaly
241.5784°
Eccentric anomaly
241.56709°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
0.00075964
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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-0702 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 | 2026-02-05 12:13:02.990Z | 12.342° NNE | 2026-02-05 12:19:02.990Z | 75.185° E | 36.76° | 2026-02-05 12:26:02.990Z | 156.516° SSE |
| 10 mins | 2026-02-05 14:04:02.990Z | 332.561° NNW | 2026-02-05 14:09:02.990Z | 280.474° WNW | 26.477° | 2026-02-05 14:14:02.990Z | 230.035° WSW |
| 12 mins | 2026-02-06 00:33:02.990Z | 153.35° SSE | 2026-02-06 00:38:02.990Z | 87.576° E | 39.11° | 2026-02-06 00:45:02.990Z | 10.184° NNE |
| 10 mins | 2026-02-06 02:24:02.990Z | 236.92° WSW | 2026-02-06 02:28:02.990Z | 277.822° WNW | 24.136° | 2026-02-06 02:34:02.990Z | 335.715° 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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