ONEWEB-0706, 61611
Orbit data source: Space-Track
ONEWEB-0706, 61611 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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61611 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: 16 hours ago
TLE from 16 hours ago
0 ONEWEB-0706
1 61611U 24188T 26207.99410344 -.00000598 00000-0 -17505-2 0 9993
2 61611 87.8822 28.3327 0002244 79.7578 280.3803 13.10372822 88595Epoch: 2026-07-26T23:51Z
TLE epoch observation values (Epoch: 2026-07-26T23:51:30.537Z)
Latitude
0.00006°
Longitude
85.77141°
Altitude
1,224.298 km
Speed
7.242 km/s
True Right ascension
01h 53m 19s
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
05:38:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,220.542 km
Perigee altitude
1,217.132 km
Semi-major axis
7,596.974 km
Eccentricity
0.00022
Inclination
87.8822°
RAAN
28.3327°
Arg. of periapsis
79.7578°
True anomaly
280.35501°
Mean anomaly
280.3803°
Eccentric anomaly
280.36765°
Mean motion
3.2778 °/min
Orbital period
109.83 mins
BSTAR
-0.0017505
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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-0706 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 | 2026-07-27 22:28:49.130Z | 39.295° NE | 2026-07-27 22:32:49.130Z | 73.076° E | 14.655° | 2026-07-27 22:35:49.130Z | 99.004° ESE |
| 13 mins | 2026-07-28 00:17:49.130Z | 359.347° N | 2026-07-28 00:23:49.130Z | 190.476° SSW | 44.946° | 2026-07-28 00:30:49.130Z | 181.871° SSW |
| 6 mins | 2026-07-28 02:09:49.130Z | 312.354° NW | 2026-07-28 02:12:49.130Z | 286.107° WNW | 14.439° | 2026-07-28 02:15:49.130Z | 260.808° W |
| 7 mins | 2026-07-28 10:50:49.130Z | 99.509° ESE | 2026-07-28 10:53:49.130Z | 71.869° E | 16.72° | 2026-07-28 10:57:49.130Z | 37.261° NE |
| 13 mins | 2026-07-28 12:36:49.130Z | 184.116° SSW | 2026-07-28 12:42:49.130Z | 276.499° WNW | 44.611° | 2026-07-28 12:49:49.130Z | 358.416° N |
| 4 mins | 2026-07-28 14:32:49.130Z | 280.389° WNW | 2026-07-28 14:33:49.130Z | 288.959° WNW | 12.501° | 2026-07-28 14:36:49.130Z | 313.696° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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