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: 9 hours ago
TLE from 9 hours ago
0 ONEWEB-0702
1 61608U 24188Q 26125.75111375 -.00000339 00000-0 -99272-3 0 9999
2 61608 87.8937 29.4189 0001067 50.2029 309.9192 13.11414473 78928Epoch: 2026-05-05T18:01Z
TLE epoch observation values (Epoch: 2026-05-05T18:01:36.228Z)
Latitude
-0.00007°
Longitude
-104.60352°
Altitude
1,220.061 km
Speed
7.245 km/s
True Right ascension
01h 57m 40s
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
10:45:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,215.621 km
Perigee altitude
1,214 km
Semi-major axis
7,592.947 km
Eccentricity
0.00011
Inclination
87.8937°
RAAN
29.4189°
Arg. of periapsis
50.2029°
True anomaly
309.90982°
Mean anomaly
309.9192°
Eccentric anomaly
309.91451°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
-0.00099272
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-06 03:50:18.587Z | 52.49° ENE | 2026-05-06 03:52:18.587Z | 68.982° E | 11.771° | 2026-05-06 03:54:18.587Z | 85.569° E |
| 13 mins | 2026-05-06 05:37:18.587Z | 3.347° NNE | 2026-05-06 05:43:18.587Z | 71.58° E | 44.216° | 2026-05-06 05:50:18.587Z | 174.758° S |
| 7 mins | 2026-05-06 07:29:18.587Z | 316.54° NNW | 2026-05-06 07:32:18.587Z | 288.832° WNW | 17.502° | 2026-05-06 07:36:18.587Z | 252.594° W |
| 5 mins | 2026-05-06 16:11:18.587Z | 88.014° E | 2026-05-06 16:13:18.587Z | 70.638° E | 13.555° | 2026-05-06 16:16:18.587Z | 45.404° ENE |
| 13 mins | 2026-05-06 17:56:18.587Z | 175.741° S | 2026-05-06 18:02:18.587Z | 39.357° NE | 44.774° | 2026-05-06 18:09:18.587Z | 1.822° NNE |
| 6 mins | 2026-05-06 19:50:18.587Z | 264.437° W | 2026-05-06 19:53:18.587Z | 291.934° WNW | 15.456° | 2026-05-06 19:56:18.587Z | 317.925° 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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