ELECTRON R/B, 65972
Orbit data source: Space-Track
ELECTRON R/B, 65972 is space debris in LEO originally from an American launch on Tue, 14 Oct 2025 UTC launched from the Rocket Lab Launch Complex (RLLC). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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65972 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ELECTRON R/B
1 65972U 25229B 25289.74404435 .02940838 70625-5 10507-2 0 9990
2 65972 41.9266 193.3565 0256487 248.7725 108.5556 15.79191384 321
Epoch: 2025-10-16T17:51Z
TLE epoch observation values (Epoch: 2025-10-16T17:51:25.431Z)
Latitude
-0°
Longitude
-99.99884°
Altitude
391.06 km
Speed
7.644 km/s
True Right ascension
12h 53m 25s
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
21:26:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.086 km
Perigee altitude
162.724 km
Semi-major axis
6,713.042 km
Eccentricity
0.02565
Inclination
41.9266°
RAAN
193.3565°
Arg. of periapsis
248.7725°
True anomaly
111.31272°
Mean anomaly
108.5556°
Eccentric anomaly
109.93709°
Mean motion
3.94606 °/min
Orbital period
91.23 mins
BSTAR
0.0010507
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Other satellites on launch #229 in the year 2025 (2025-10-14 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.ELECTRON R/B 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. |
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4 mins | 2025-10-18 19:57:22.559Z | 190.223° SSW | 2025-10-18 19:59:22.559Z | 144.759° SSE | 20.138° | 2025-10-18 20:01:22.559Z | 102.855° ESE |
5 mins | 2025-10-18 21:32:22.559Z | 249.123° W | 2025-10-18 21:34:22.559Z | 90.576° ESE | 42.843° | 2025-10-18 21:37:22.559Z | 76.037° E |
5 mins | 2025-10-18 23:07:22.559Z | 288.034° WNW | 2025-10-18 23:09:22.559Z | 24.018° NE | 40.226° | 2025-10-18 23:12:22.559Z | 81.043° E |
5 mins | 2025-10-19 00:42:22.559Z | 281.594° WNW | 2025-10-19 00:44:22.559Z | 153.568° SSE | 44.206° | 2025-10-19 00:47:22.559Z | 110.541° ESE |
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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