ELECTRON KICK STAGE R/B, 68100
Orbit data source: Space-Track
ELECTRON KICK STAGE R/B, 68100 is space debris in LEO originally from an American 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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USExpand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 ELECTRON KICK STAGE R/B
1 68100U 26043C 26066.53447938 .02414689 79320-5 21065-2 0 9999
2 68100 42.1237 87.3350 0186570 32.3846 328.8306 15.85533381 232Epoch: 2026-03-07T12:49Z
TLE epoch observation values (Epoch: 2026-03-07T12:49:39.018Z)
Latitude
-0.00005°
Longitude
89.66763°
Altitude
208.303 km
Speed
7.845 km/s
True Right ascension
05h 49m 20s
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
03:09:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.879 km
Perigee altitude
192.058 km
Semi-major axis
6,695.106 km
Eccentricity
0.01866
Inclination
42.1237°
RAAN
87.335°
Arg. of periapsis
32.3846°
True anomaly
327.70163°
Mean anomaly
328.8306°
Eccentric anomaly
328.26839°
Mean motion
3.96193 °/min
Orbital period
90.86 mins
BSTAR
0.0021065
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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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| ELECTRON KICK STAGE 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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