ELECTRON KICK STAGE R/B, 68100 (Decayed)
Orbit data source: Space-Track
ELECTRON KICK STAGE R/B, 68100 was space debris in LEO originally from a launch on Thu, 05 Mar 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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68100 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
Unknown shape, 8.0 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 ELECTRON KICK STAGE R/B
1 68100U 26043C 26071.39923850 .08447794 86167-5 14187-2 0 9994
2 68100 42.1107 56.2036 0067147 72.1355 288.6827 16.25407189 1018Epoch: 2026-03-12T09:34Z
TLE epoch observation values (Epoch: 2026-03-12T09:34:54.206Z)
Latitude
-0°
Longitude
102.42806°
Altitude
190.684 km
Speed
7.802 km/s
True Right ascension
03h 44m 48s
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
06:48:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
251.312 km
Perigee altitude
162.876 km
Semi-major axis
6,585.231 km
Eccentricity
0.00671
Inclination
42.1107°
RAAN
56.2036°
Arg. of periapsis
72.1355°
True anomaly
287.95185°
Mean anomaly
288.6827°
Eccentric anomaly
288.31747°
Mean motion
4.0615 °/min
Orbital period
88.64 mins
BSTAR
0.0014187
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Other satellites on launch #43 in the year 2026 (2026-03-05 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 KICK STAGE 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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