ELECTRON R/B, 100683
Orbit data source: Space-Track
ELECTRON R/B, 100683 is space debris in LEO originally from an American launch on Fri, 11 Sep 2026 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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100683 intel report (Beta)
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USExpand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 ELECTRON R/B
1 A0683U 26207B 26255.55842767 .01460877 26335-5 14588-2 0 9993
2 A0683 36.0696 302.1089 0212194 49.1608 312.7331 15.78511294 226Epoch: 2026-09-12T13:24Z
TLE epoch observation values (Epoch: 2026-09-12T13:24:08.150Z)
Latitude
-0.00003°
Longitude
109.50919°
Altitude
238.682 km
Speed
7.821 km/s
True Right ascension
20h 08m 26s
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
20:48:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
480.323 km
Perigee altitude
195.306 km
Semi-major axis
6,715.952 km
Eccentricity
0.02122
Inclination
36.0696°
RAAN
302.1089°
Arg. of periapsis
49.1608°
True anomaly
310.91466°
Mean anomaly
312.7331°
Eccentric anomaly
311.82715°
Mean motion
3.9435 °/min
Orbital period
91.29 mins
BSTAR
0.0014588
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Other satellites on launch #207 in the year 2026 (2026-09-11 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
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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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| ELECTRON R/B is likely not visible in the next few days. |
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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