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, 2.5 m
Radar Cross Section
2.032 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 ONEWEB-0705
1 61610U 24188S 25260.01999209 -.00000655 00000-0 -19121-2 0 9995
2 61610 87.8745 90.7169 0002734 103.4605 256.6827 13.10372210 39684Epoch: 2025-09-17T00:28Z
TLE epoch observation values (Epoch: 2025-09-17T00:28:47.316Z)
Latitude
-0.00004°
Longitude
87.31781°
Altitude
1,225.086 km
Speed
7.242 km/s
True Right ascension
06h 02m 52s
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
09:16:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,220.916 km
Perigee altitude
1,216.762 km
Semi-major axis
7,596.976 km
Eccentricity
0.00027
Inclination
87.8745°
RAAN
90.7169°
Arg. of periapsis
103.4605°
True anomaly
256.65222°
Mean anomaly
256.6827°
Eccentric anomaly
256.66746°
Mean motion
3.2778 °/min
Orbital period
109.83 mins
BSTAR
-0.0019121
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-17 23:06:59.134Z | 46.784° ENE | 2025-09-17 23:09:59.134Z | 71.98° E | 13.057° | 2025-09-17 23:12:59.134Z | 96.795° ESE |
| 13 mins | 2025-09-18 00:54:59.134Z | 1.676° NNE | 2025-09-18 01:00:59.134Z | 99.402° ESE | 44.796° | 2025-09-18 01:07:59.134Z | 178.098° S |
| 7 mins | 2025-09-18 02:46:59.134Z | 314.232° NW | 2025-09-18 02:49:59.134Z | 287.096° WNW | 16.098° | 2025-09-18 02:53:59.134Z | 252.953° W |
| 6 mins | 2025-09-18 11:28:59.134Z | 90.976° ESE | 2025-09-18 11:30:59.134Z | 72.983° E | 15.038° | 2025-09-18 11:34:59.134Z | 39.187° NE |
| 13 mins | 2025-09-18 13:13:59.134Z | 179.74° S | 2025-09-18 13:19:59.134Z | 235.46° WSW | 44.974° | 2025-09-18 13:26:59.134Z | 0.187° NNE |
| 5 mins | 2025-09-18 15:08:59.134Z | 270.258° WNW | 2025-09-18 15:10:59.134Z | 287.879° WNW | 14.08° | 2025-09-18 15:13:59.134Z | 313.703° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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