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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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: 15 hours ago
TLE from 15 hours ago
0 ONEWEB-0695
1 61602U 24188J 26277.75463899 .00000511 00000-0 14068-2 0 9991
2 61602 87.8959 359.3000 0001649 118.4327 241.6967 13.11418502 98827Epoch: 2026-10-04T18:06Z
TLE epoch observation values (Epoch: 2026-10-04T18:06:40.808Z)
Latitude
-0.00006°
Longitude
74.18662°
Altitude
1,221.16 km
Speed
7.244 km/s
True Right ascension
23h 57m 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
03:02:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,216.047 km
Perigee altitude
1,213.543 km
Semi-major axis
7,592.932 km
Eccentricity
0.00016
Inclination
87.8959°
RAAN
359.3°
Arg. of periapsis
118.4327°
True anomaly
241.68006°
Mean anomaly
241.6967°
Eccentric anomaly
241.68838°
Mean motion
3.28042 °/min
Orbital period
109.74 mins
BSTAR
0.0014068
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-10-05 16:41:34.496Z | 20.526° NNE | 2026-10-05 16:47:34.496Z | 81.209° E | 32.786° | 2026-10-05 16:53:34.496Z | 140.093° SSE |
| 12 mins | 2026-10-05 18:31:34.496Z | 343.631° N | 2026-10-05 18:37:34.496Z | 275.862° WNW | 44.503° | 2026-10-05 18:43:34.496Z | 211.326° SW |
| 11 mins | 2026-10-06 05:01:34.496Z | 136.667° SSE | 2026-10-06 05:06:34.496Z | 80.493° E | 36.701° | 2026-10-06 05:12:34.496Z | 19.227° NNE |
| 12 mins | 2026-10-06 06:50:34.496Z | 214.262° SW | 2026-10-06 06:56:34.496Z | 282.048° WNW | 39.751° | 2026-10-06 07:02:34.496Z | 343.661° 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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