ELECTRON KICK STAGE R/B, 64341 (Decayed)
Orbit data source: Space-Track
ELECTRON KICK STAGE R/B, 64341 was space debris in LEO originally from a launch on Wed, 11 Jun 2025 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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64341 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
Trunc Cone, 8.0 m
Radar Cross Section
0.760 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 months ago
TLE from 8 months ago
0 ELECTRON KICK STAGE R/B
1 64341U 25125B 25259.99996905 .05595691 81367-5 15952-2 0 9996
2 64341 41.9866 196.0799 0038555 243.3120 116.3800 16.24325627 15256Epoch: 2025-09-16T23:59Z
TLE epoch observation values (Epoch: 2025-09-16T23:59:57.325Z)
Latitude
-0.00006°
Longitude
-160.09122°
Altitude
218.841 km
Speed
7.771 km/s
True Right ascension
13h 04m 19s
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
23:47:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
235.437 km
Perigee altitude
184.636 km
Semi-major axis
6,588.173 km
Eccentricity
0.00386
Inclination
41.9866°
RAAN
196.0799°
Arg. of periapsis
243.312°
True anomaly
116.77495°
Mean anomaly
116.38°
Eccentric anomaly
116.57756°
Mean motion
4.05878 °/min
Orbital period
88.7 mins
BSTAR
0.0015952
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Other satellites on launch #125 in the year 2025 (2025-06-11 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 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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