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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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: 1 day ago
TLE from 1 day ago
0 ONEWEB-0706
1 61611U 24188T 25305.43778752 .00000327 00000-0 90094-3 0 9993
2 61611 87.8787 81.6708 0002045 80.9868 279.1491 13.10374625 53555Epoch: 2025-11-01T10:30Z
TLE epoch observation values (Epoch: 2025-11-01T10:30:24.841Z)
Latitude
-0.00001°
Longitude
-116.90058°
Altitude
1,224.351 km
Speed
7.242 km/s
True Right ascension
05h 26m 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
07:42:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,220.384 km
Perigee altitude
1,217.276 km
Semi-major axis
7,596.967 km
Eccentricity
0.0002
Inclination
87.8787°
RAAN
81.6708°
Arg. of periapsis
80.9868°
True anomaly
279.12596°
Mean anomaly
279.1491°
Eccentric anomaly
279.13753°
Mean motion
3.2778 °/min
Orbital period
109.83 mins
BSTAR
0.00090094
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-11-02 20:06:39.230Z | 26.906° NE | 2025-11-02 20:11:39.230Z | 75.148° E | 24.215° | 2025-11-02 20:17:39.230Z | 131.872° SE |
| 12 mins | 2025-11-02 21:56:39.230Z | 346.29° N | 2025-11-02 22:02:39.230Z | 261.834° W | 38.828° | 2025-11-02 22:08:39.230Z | 202.586° SW |
| 10 mins | 2025-11-03 08:27:39.230Z | 124.785° SE | 2025-11-03 08:31:39.230Z | 81.408° E | 26.674° | 2025-11-03 08:37:39.230Z | 22.775° NE |
| 12 mins | 2025-11-03 10:15:39.230Z | 206.45° SW | 2025-11-03 10:21:39.230Z | 279.44° WNW | 36.738° | 2025-11-03 10:27:39.230Z | 346.717° N |
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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