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 26216.69687794 -.00000359 00000-0 -10497-2 0 9999
2 61608 87.8930 11.3370 0002618 76.8487 283.2933 13.11418316 90840Epoch: 2026-08-04T16:43Z
TLE epoch observation values (Epoch: 2026-08-04T16:43:30.254Z)
Latitude
0.00001°
Longitude
167.19902°
Altitude
1,220.11 km
Speed
7.245 km/s
True Right ascension
00h 45m 20s
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
06:27:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.783 km
Perigee altitude
1,212.808 km
Semi-major axis
7,592.933 km
Eccentricity
0.00026
Inclination
87.893°
RAAN
11.337°
Arg. of periapsis
76.8487°
True anomaly
283.2641°
Mean anomaly
283.2933°
Eccentric anomaly
283.2787°
Mean motion
3.28042 °/min
Orbital period
109.74 mins
BSTAR
-0.0010497
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-05 20:49:54.969Z | 42.903° NE | 2026-08-05 20:52:54.969Z | 69.175° E | 15.577° | 2026-08-05 20:56:54.969Z | 104.399° ESE |
| 13 mins | 2026-08-05 22:37:54.969Z | 357.947° N | 2026-08-05 22:43:54.969Z | 302.28° NW | 44.846° | 2026-08-05 22:50:54.969Z | 184.203° SSW |
| 5 mins | 2026-08-06 00:30:54.969Z | 305.737° NW | 2026-08-06 00:32:54.969Z | 288.306° WNW | 13.461° | 2026-08-06 00:35:54.969Z | 263.342° W |
| 7 mins | 2026-08-06 09:10:54.969Z | 98.882° ESE | 2026-08-06 09:13:54.969Z | 70.03° E | 17.545° | 2026-08-06 09:17:54.969Z | 35.406° NE |
| 13 mins | 2026-08-06 10:56:54.969Z | 186.689° SSW | 2026-08-06 11:02:54.969Z | 296.424° NW | 44.073° | 2026-08-06 11:09:54.969Z | 357.729° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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