ONEWEB-0701, 61607
Orbit data source: Space-Track
ONEWEB-0701, 61607 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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61607 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: 9 hours ago
TLE from 9 hours ago
0 ONEWEB-0701
1 61607U 24188P 26305.90647707 -.00000675 00000-0 -19714-2 0 9993
2 61607 87.8899 8.8827 0001961 123.0727 237.0589 13.10373792101342Epoch: 2026-11-01T21:45Z
TLE epoch observation values (Epoch: 2026-11-01T21:45:19.618Z)
Latitude
-0.00003°
Longitude
1.35983°
Altitude
1,225.412 km
Speed
7.241 km/s
True Right ascension
00h 35m 31s
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
02:31:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,220.323 km
Perigee altitude
1,217.343 km
Semi-major axis
7,596.97 km
Eccentricity
0.0002
Inclination
87.8899°
RAAN
8.8827°
Arg. of periapsis
123.0727°
True anomaly
237.04004°
Mean anomaly
237.0589°
Eccentric anomaly
237.04947°
Mean motion
3.2778 °/min
Orbital period
109.83 mins
BSTAR
-0.0019714
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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-0701 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-11-02 14:52:51.382Z | 38.509° NE | 2026-11-02 14:56:51.382Z | 73.668° E | 17.241° | 2026-11-02 15:00:51.382Z | 108.523° ESE |
| 13 mins | 2026-11-02 16:41:51.382Z | 356.702° N | 2026-11-02 16:47:51.382Z | 242.797° WSW | 80.298° | 2026-11-02 16:54:51.382Z | 185.876° SSW |
| 4 mins | 2026-11-02 18:34:51.382Z | 302.976° NW | 2026-11-02 18:35:51.382Z | 294.477° NW | 13.074° | 2026-11-02 18:38:51.382Z | 269.267° W |
| 8 mins | 2026-11-03 03:13:51.382Z | 108.208° ESE | 2026-11-03 03:17:51.382Z | 70.668° E | 19.741° | 2026-11-03 03:21:51.382Z | 35.253° NE |
| 13 mins | 2026-11-03 05:00:51.382Z | 188.947° SSW | 2026-11-03 05:06:51.382Z | 281.323° WNW | 72.772° | 2026-11-03 05:13:51.382Z | 356.573° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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