ONEWEB-0700, 61606
Orbit data source: Space-Track
ONEWEB-0700, 61606 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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61606 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-0700
1 61606U 24188N 25291.85110646 -.00000345 00000-0 -10237-2 0 9991
2 61606 87.8774 84.2513 0002343 88.5060 271.6336 13.10373959 51694Epoch: 2025-10-18T20:25Z
TLE epoch observation values (Epoch: 2025-10-18T20:25:35.598Z)
Latitude
0.00002°
Longitude
110.27678°
Altitude
1,224.55 km
Speed
7.242 km/s
True Right ascension
05h 37m 00s
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
19:42:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,220.613 km
Perigee altitude
1,217.053 km
Semi-major axis
7,596.97 km
Eccentricity
0.00023
Inclination
87.8774°
RAAN
84.2513°
Arg. of periapsis
88.506°
True anomaly
271.60676°
Mean anomaly
271.6336°
Eccentric anomaly
271.62018°
Mean motion
3.2778 °/min
Orbital period
109.83 mins
BSTAR
-0.0010237
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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-0700 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-10-20 09:13:11.193Z | 115.537° SE | 2025-10-20 09:17:11.193Z | 79.049° E | 20.182° | 2025-10-20 09:22:11.193Z | 32.549° NE |
| 12 mins | 2025-10-20 11:01:11.193Z | 193.31° SSW | 2025-10-20 11:07:11.193Z | 289.456° WNW | 42.411° | 2025-10-20 11:13:11.193Z | 353.704° N |
| 7 mins | 2025-10-20 20:43:11.193Z | 45.034° ENE | 2025-10-20 20:46:11.193Z | 72.329° E | 16.386° | 2025-10-20 20:50:11.193Z | 107.501° ESE |
| 13 mins | 2025-10-20 22:31:11.193Z | 356.85° N | 2025-10-20 22:37:11.193Z | 258.316° W | 44.687° | 2025-10-20 22:44:11.193Z | 185.755° SSW |
| 4 mins | 2025-10-21 00:24:11.193Z | 304.148° NW | 2025-10-21 00:26:11.193Z | 286.977° WNW | 12.788° | 2025-10-21 00:28:11.193Z | 270.271° WNW |
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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