ELECTRON KICK STAGE R/B, 68411 (Decayed)
Orbit data source: Space-Track
ELECTRON KICK STAGE R/B, 68411 was space debris in LEO originally from a launch on Sat, 28 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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68411 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
KICK STAGE, CURIE
Mass
~42 kg wet, ~42 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 8.0 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 ELECTRON KICK STAGE R/B
1 68411U 26065D 26106.16404788 .05715083 26561-5 15668-3 0 9995
2 68411 97.3981 350.2379 0037444 307.1011 52.6868 16.40761515 3007Epoch: 2026-04-16T03:56Z
TLE epoch observation values (Epoch: 2026-04-16T03:56:13.736Z)
Latitude
-0.00007°
Longitude
86.86515°
Altitude
152.236 km
Speed
7.824 km/s
True Right ascension
23h 20m 57s
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
10:19:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
185.068 km
Perigee altitude
136.1 km
Semi-major axis
6,538.721 km
Eccentricity
0.00374
Inclination
97.3981°
RAAN
350.2379°
Arg. of periapsis
307.1011°
True anomaly
53.02903°
Mean anomaly
52.6868°
Eccentric anomaly
52.85782°
Mean motion
4.10491 °/min
Orbital period
87.7 mins
BSTAR
0.00015668
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Other satellites on launch #65 in the year 2026 (2026-03-28 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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