ONEWEB-0695, 61602
Orbit data source: Space-Track
ONEWEB-0695, 61602 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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61602 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, 2.5 m
Radar Cross Section
2.032 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 ONEWEB-0695
1 61602U 24188J 25260.88928576 -.00000362 00000-0 -10571-2 0 9995
2 61602 87.8773 75.3328 0001975 106.9254 253.2091 13.11414421 48774Epoch: 2025-09-17T21:20Z
TLE epoch observation values (Epoch: 2025-09-17T21:20:34.289Z)
Latitude
0.00001°
Longitude
118.13117°
Altitude
1,221.015 km
Speed
7.244 km/s
True Right ascension
05h 01m 19s
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
03:59:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.31 km
Perigee altitude
1,213.311 km
Semi-major axis
7,592.948 km
Eccentricity
0.0002
Inclination
87.8773°
RAAN
75.3328°
Arg. of periapsis
106.9254°
True anomaly
253.18743°
Mean anomaly
253.2091°
Eccentric anomaly
253.19827°
Mean motion
3.28041 °/min
Orbital period
109.74 mins
BSTAR
-0.0010571
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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-0695 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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2025-09-18 12:05:13.630Z | 174.549° S | 2025-09-18 12:11:13.630Z | 140.107° SSE | 44.412° | 2025-09-18 12:18:13.630Z | 2.595° NNE |
| 7 mins | 2025-09-18 13:59:13.630Z | 258.181° W | 2025-09-18 14:02:13.630Z | 285.086° WNW | 16.101° | 2025-09-18 14:06:13.630Z | 320.427° NNW |
| 13 mins | 2025-09-18 23:35:13.630Z | 6.544° NNE | 2025-09-18 23:41:13.630Z | 79.255° E | 42.63° | 2025-09-18 23:48:13.630Z | 169.15° S |
| 8 mins | 2025-09-19 01:27:13.630Z | 318.335° NNW | 2025-09-19 01:30:13.630Z | 288.976° WNW | 20.072° | 2025-09-19 01:35:13.630Z | 242.735° WSW |
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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