ONEWEB-0688, 61596
Orbit data source: Space-Track
ONEWEB-0688, 61596 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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61596 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: 8 hours ago
TLE from 8 hours ago
0 ONEWEB-0688
1 61596U 24188C 25346.91210064 -.00000004 00000-0 -43614-4 0 9991
2 61596 87.9098 42.9374 0002507 130.9673 229.1676 13.17647125 61368Epoch: 2025-12-12T21:53Z
TLE epoch observation values (Epoch: 2025-12-12T21:53:25.495Z)
Latitude
0.00001°
Longitude
-7.26575°
Altitude
1,197.861 km
Speed
7.254 km/s
True Right ascension
02h 51m 44s
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
03:57:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,192.727 km
Perigee altitude
1,188.932 km
Semi-major axis
7,568.966 km
Eccentricity
0.00025
Inclination
87.9098°
RAAN
42.9374°
Arg. of periapsis
130.9673°
True anomaly
229.14587°
Mean anomaly
229.1676°
Eccentric anomaly
229.15673°
Mean motion
3.29601 °/min
Orbital period
109.22 mins
BSTAR
-0.000043614
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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-0688 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 | 2025-12-13 14:55:37.832Z | 34.308° NE | 2025-12-13 14:59:37.832Z | 78.298° E | 24.724° | 2025-12-13 15:04:37.832Z | 129.069° SE |
| 12 mins | 2025-12-13 16:43:37.832Z | 346.09° N | 2025-12-13 16:49:37.832Z | 266.596° W | 38.077° | 2025-12-13 16:55:37.832Z | 204.183° SW |
| 10 mins | 2025-12-14 03:10:37.832Z | 128.707° SE | 2025-12-14 03:15:37.832Z | 76.823° E | 25.96° | 2025-12-14 03:20:37.832Z | 26.369° NE |
| 12 mins | 2025-12-14 04:58:37.832Z | 205.016° SW | 2025-12-14 05:04:37.832Z | 277.768° WNW | 37.083° | 2025-12-14 05:10:37.832Z | 347.096° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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