ELECTRON R/B, 100683
Orbit data source: Space-Track
ELECTRON R/B, 100683 is space debris in LEO originally from a 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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Identifier
Orbit
Country
USRelated business
Manufacturer
Rocket Lab
Mission
Spacecraft
Bus & Motor
ELECTRON ST2, Unknown motor
Mass
250 kg wet, ~250 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
CYL, 1.2 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 ELECTRON R/B
1 A0683U 26207B 26259.46507102 .02063000 26704-5 15268-2 0 9992
2 A0683 36.0713 275.5207 0167219 87.0596 274.9282 15.91285781 841Epoch: 2026-09-16T11:09Z
TLE epoch observation values (Epoch: 2026-09-16T11:09:42.136Z)
Latitude
0°
Longitude
112.67886°
Altitude
289.941 km
Speed
7.74 km/s
True Right ascension
18h 22m 04s
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
02:01:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
413.559 km
Perigee altitude
190.154 km
Semi-major axis
6,679.993 km
Eccentricity
0.01672
Inclination
36.0713°
RAAN
275.5207°
Arg. of periapsis
87.0596°
True anomaly
273.01602°
Mean anomaly
274.9282°
Eccentric anomaly
273.97241°
Mean motion
3.97538 °/min
Orbital period
90.56 mins
BSTAR
0.0015268
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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
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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