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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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: 1 day ago
TLE from 1 day ago
0 ONEWEB-0702
1 61608U 24188Q 26170.61361436 -.00000719 00000-0 -20642-2 0 9995
2 61608 87.8902 20.5041 0002211 114.0455 246.0904 13.11417196 84804Epoch: 2026-06-19T14:43Z
TLE epoch observation values (Epoch: 2026-06-19T14:43:36.280Z)
Latitude
-0.00008°
Longitude
-108.23714°
Altitude
1,221.252 km
Speed
7.243 km/s
True Right ascension
01h 22m 00s
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
07:19:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.479 km
Perigee altitude
1,213.121 km
Semi-major axis
7,592.937 km
Eccentricity
0.00022
Inclination
87.8902°
RAAN
20.5041°
Arg. of periapsis
114.0455°
True anomaly
246.06724°
Mean anomaly
246.0904°
Eccentric anomaly
246.07882°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
-0.0020642
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-21 00:20:04.333Z | 47.541° ENE | 2026-06-21 00:23:04.333Z | 73.306° E | 13.609° | 2026-06-21 00:26:04.333Z | 98.425° ESE |
| 13 mins | 2026-06-21 02:08:04.333Z | 0.913° NNE | 2026-06-21 02:14:04.333Z | 146.485° SSE | 44.781° | 2026-06-21 02:21:04.333Z | 179.637° S |
| 6 mins | 2026-06-21 04:00:04.333Z | 311.319° NW | 2026-06-21 04:03:04.333Z | 284.074° WNW | 15.355° | 2026-06-21 04:06:04.333Z | 258.337° W |
| 6 mins | 2026-06-21 12:41:04.333Z | 93.531° ESE | 2026-06-21 12:43:04.333Z | 75.492° E | 15.46° | 2026-06-21 12:47:04.333Z | 40.649° NE |
| 13 mins | 2026-06-21 14:26:04.333Z | 180.938° SSW | 2026-06-21 14:32:04.333Z | 220.727° SW | 44.814° | 2026-06-21 14:39:04.333Z | 359.526° N |
| 5 mins | 2026-06-21 16:21:04.333Z | 269.812° W | 2026-06-21 16:23:04.333Z | 287.116° WNW | 13.554° | 2026-06-21 16:26:04.333Z | 312.776° NW |
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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