ELECTRON KICK STAGE R/B, 64057 (Decayed)
Orbit data source: Space-Track
ELECTRON KICK STAGE R/B, 64057 was space debris in LEO originally from a launch on Sat, 17 May 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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64057 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, 0.8 m
Radar Cross Section
0.760 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 months ago
TLE from 9 months ago
0 ELECTRON KICK STAGE R/B
1 64057U 25104C 25261.38683556 .02837246 81443-5 18399-2 0 9993
2 64057 41.9846 264.2583 0039091 87.9093 272.6249 16.14435489 19045Epoch: 2025-09-18T09:17Z
TLE epoch observation values (Epoch: 2025-09-18T09:17:02.592Z)
Latitude
-0.00005°
Longitude
127.44828°
Altitude
233.27 km
Speed
7.769 km/s
True Right ascension
17h 37m 01s
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
07:19:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
262.757 km
Perigee altitude
211.039 km
Semi-major axis
6,615.035 km
Eccentricity
0.00391
Inclination
41.9846°
RAAN
264.2583°
Arg. of periapsis
87.9093°
True anomaly
272.17732°
Mean anomaly
272.6249°
Eccentric anomaly
272.40112°
Mean motion
4.03408 °/min
Orbital period
89.24 mins
BSTAR
0.0018399
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Other satellites on launch #104 in the year 2025 (2025-05-17 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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