ONEWEB-0687, 61595
Orbit data source: Space-Track
ONEWEB-0687, 61595 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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61595 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-0687
1 61595U 24188B 25306.33350098 .00000009 00000-0 -88835-5 0 9993
2 61595 87.9109 51.0128 0001517 81.0132 279.1171 13.17651564 56028Epoch: 2025-11-02T08:00Z
TLE epoch observation values (Epoch: 2025-11-02T08:00:14.484Z)
Latitude
-0.00005°
Longitude
-110.89828°
Altitude
1,196.42 km
Speed
7.256 km/s
True Right ascension
03h 24m 03s
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
05:30:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,191.96 km
Perigee altitude
1,189.664 km
Semi-major axis
7,568.949 km
Eccentricity
0.00015
Inclination
87.9109°
RAAN
51.0128°
Arg. of periapsis
81.0132°
True anomaly
279.09994°
Mean anomaly
279.1171°
Eccentric anomaly
279.10852°
Mean motion
3.29602 °/min
Orbital period
109.22 mins
BSTAR
-0.0000088835
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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-0687 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-03 17:27:40.545Z | 51.435° ENE | 2025-11-03 17:29:40.545Z | 68.922° E | 13.511° | 2025-11-03 17:32:40.545Z | 95.018° ESE |
| 12 mins | 2025-11-03 19:14:40.545Z | 0.745° NNE | 2025-11-03 19:20:40.545Z | 153.62° SSE | 44.746° | 2025-11-03 19:26:40.545Z | 179.622° S |
| 5 mins | 2025-11-03 21:06:40.545Z | 306.773° NW | 2025-11-03 21:08:40.545Z | 288.31° WNW | 15.091° | 2025-11-03 21:11:40.545Z | 261.587° W |
| 6 mins | 2025-11-04 05:44:40.545Z | 93.011° ESE | 2025-11-04 05:46:40.545Z | 75.247° E | 14.453° | 2025-11-04 05:50:40.545Z | 40.788° NE |
| 12 mins | 2025-11-04 07:29:40.545Z | 179.069° S | 2025-11-04 07:35:40.545Z | 351.799° N | 44.836° | 2025-11-04 07:41:40.545Z | 0.297° NNE |
| 5 mins | 2025-11-04 09:23:40.545Z | 269.668° W | 2025-11-04 09:25:40.545Z | 287.612° WNW | 14.081° | 2025-11-04 09:28:40.545Z | 313.859° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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