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: 11 hours ago
TLE from 11 hours ago
0 ONEWEB-0702
1 61608U 24188Q 25352.57766819 .00000085 00000-0 20324-3 0 9997
2 61608 87.8825 56.9376 0000808 77.8325 282.2894 13.11413222 60815Epoch: 2025-12-18T13:51Z
TLE epoch observation values (Epoch: 2025-12-18T13:51:50.531Z)
Latitude
0.00003°
Longitude
121.54588°
Altitude
1,220.456 km
Speed
7.244 km/s
True Right ascension
03h 47m 45s
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
00:03:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,215.429 km
Perigee altitude
1,214.202 km
Semi-major axis
7,592.952 km
Eccentricity
0.00008
Inclination
87.8825°
RAAN
56.9376°
Arg. of periapsis
77.8325°
True anomaly
282.28035°
Mean anomaly
282.2894°
Eccentric anomaly
282.28488°
Mean motion
3.2804 °/min
Orbital period
109.74 mins
BSTAR
0.00020324
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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 | 2025-12-19 04:36:31.488Z | 165.731° S | 2025-12-19 04:42:31.488Z | 107.971° ESE | 42.372° | 2025-12-19 04:49:31.488Z | 6.952° NNE |
| 9 mins | 2025-12-19 06:29:31.488Z | 246.563° WSW | 2025-12-19 06:33:31.488Z | 285.227° WNW | 20.027° | 2025-12-19 06:38:31.488Z | 330.193° NNW |
| 13 mins | 2025-12-19 16:06:31.488Z | 11.304° NNE | 2025-12-19 16:12:31.488Z | 82.453° E | 38.968° | 2025-12-19 16:19:31.488Z | 161.031° S |
| 10 mins | 2025-12-19 17:57:31.488Z | 328.885° NNW | 2025-12-19 18:02:31.488Z | 276.618° WNW | 24.251° | 2025-12-19 18:07:31.488Z | 231.282° WSW |
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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