ONEWEB-0705, 61610
Orbit data source: Space-Track
ONEWEB-0705, 61610 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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61610 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: 9 hours ago
TLE from 9 hours ago
0 ONEWEB-0705
1 61610U 24188S 25299.64954453 -.00000382 00000-0 -11303-2 0 9999
2 61610 87.8773 82.8012 0002338 66.8611 293.2762 13.10371931 44874Epoch: 2025-10-26T15:35Z
TLE epoch observation values (Epoch: 2025-10-26T15:35:20.647Z)
Latitude
-0.00007°
Longitude
173.70246°
Altitude
1,223.906 km
Speed
7.243 km/s
True Right ascension
05h 31m 12s
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
20:23:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,220.617 km
Perigee altitude
1,217.064 km
Semi-major axis
7,596.977 km
Eccentricity
0.00023
Inclination
87.8773°
RAAN
82.8012°
Arg. of periapsis
66.8611°
True anomaly
293.25159°
Mean anomaly
293.2762°
Eccentric anomaly
293.26389°
Mean motion
3.2778 °/min
Orbital period
109.83 mins
BSTAR
-0.0011303
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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-0705 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-27 08:15:42.460Z | 91.732° ESE | 2025-10-27 08:18:42.460Z | 66.58° ENE | 12.752° | 2025-10-27 08:20:42.460Z | 49.927° ENE |
| 12 mins | 2025-10-27 10:01:42.460Z | 173.289° S | 2025-10-27 10:06:42.460Z | 129.336° SE | 44.47° | 2025-10-27 10:13:42.460Z | 2.87° NNE |
| 7 mins | 2025-10-27 11:54:42.460Z | 258.016° W | 2025-10-27 11:57:42.460Z | 285.123° WNW | 16.385° | 2025-10-27 12:01:42.460Z | 320.613° NNW |
| 12 mins | 2025-10-27 21:31:42.460Z | 7.884° NNE | 2025-10-27 21:37:42.460Z | 105.147° ESE | 42.371° | 2025-10-27 21:43:42.460Z | 168.127° S |
| 9 mins | 2025-10-27 23:22:42.460Z | 322.48° NNW | 2025-10-27 23:26:42.460Z | 283.87° WNW | 20.285° | 2025-10-27 23:31:42.460Z | 239.882° WSW |
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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