ONEWEB-0691, 61599
Orbit data source: Space-Track
ONEWEB-0691, 61599 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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61599 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-0691
1 61599U 24188F 26208.02278070 -.00000498 00000-0 -14417-2 0 9999
2 61599 87.8914 13.0463 0001452 85.2651 274.8643 13.11416277 89706Epoch: 2026-07-27T00:32Z
TLE epoch observation values (Epoch: 2026-07-27T00:32:48.252Z)
Latitude
0°
Longitude
60.13293°
Altitude
1,220.481 km
Speed
7.244 km/s
True Right ascension
00h 52m 11s
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
1,215.906 km
Perigee altitude
1,213.701 km
Semi-major axis
7,592.94 km
Eccentricity
0.00015
Inclination
87.8914°
RAAN
13.0463°
Arg. of periapsis
85.2651°
True anomaly
274.84772°
Mean anomaly
274.8643°
Eccentric anomaly
274.85601°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
-0.0014417
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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-0691 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-07-27 21:20:48.801Z | 53.035° ENE | 2026-07-27 21:22:48.801Z | 69.846° E | 12.36° | 2026-07-27 21:24:48.801Z | 86.705° E |
| 13 mins | 2026-07-27 23:07:48.801Z | 2.576° NNE | 2026-07-27 23:13:48.801Z | 78.056° E | 44.55° | 2026-07-27 23:20:48.801Z | 176.353° S |
| 7 mins | 2026-07-28 00:59:48.801Z | 315.286° NNW | 2026-07-28 01:02:48.801Z | 287.771° WNW | 16.827° | 2026-07-28 01:06:48.801Z | 252.592° W |
| 5 mins | 2026-07-28 09:41:48.801Z | 87.532° E | 2026-07-28 09:43:48.801Z | 69.725° E | 14.169° | 2026-07-28 09:46:48.801Z | 44.297° NE |
| 12 mins | 2026-07-28 11:26:48.801Z | 177.49° S | 2026-07-28 11:32:48.801Z | 12.583° NNE | 44.738° | 2026-07-28 11:38:48.801Z | 1.074° NNE |
| 6 mins | 2026-07-28 13:20:48.801Z | 265.747° W | 2026-07-28 13:22:48.801Z | 283.463° WNW | 14.807° | 2026-07-28 13:26:48.801Z | 318.243° NNW |
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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