ELECTRON R/B, 100683 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 100683 was 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
Decayed 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, 8.0 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 3 weeks ago
TLE from 3 weeks ago
0 ELECTRON R/B
1 A0683U 26207B 26265.17777301 .18904296 24234-5 32012-3 0 9998
2 A0683 36.0579 235.2748 0028501 141.2210 219.0614 16.44887046 1762Epoch: 2026-09-22T04:15Z
TLE epoch observation values (Epoch: 2026-09-22T04:15:59.588Z)
Latitude
0°
Longitude
170.22954°
Altitude
166.272 km
Speed
7.8 km/s
True Right ascension
15h 41m 05s
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
15:13:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
174.702 km
Perigee altitude
137.456 km
Semi-major axis
6,534.216 km
Eccentricity
0.00285
Inclination
36.0579°
RAAN
235.2748°
Arg. of periapsis
141.221°
True anomaly
218.85616°
Mean anomaly
219.0614°
Eccentric anomaly
218.95872°
Mean motion
4.10916 °/min
Orbital period
87.61 mins
BSTAR
0.00032012
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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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| This satellite is decayed. |
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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