ELECTRON KICK STAGE R/B, 64625 (Decayed)
Orbit data source: Space-Track
ELECTRON KICK STAGE R/B, 64625 was space debris in LEO originally from a launch on Thu, 26 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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64625 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
KICK STAGE, CURIE
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Trunc Cone, 0.7 m
Radar Cross Section
0.760 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 ELECTRON KICK STAGE R/B
1 64625U 25138E 25182.76837584 .22805110 15550-5 24288-3 0 9995
2 64625 97.3030 187.9056 0067877 204.0553 212.3610 16.41889293 788Epoch: 2025-07-01T18:26Z
TLE epoch observation values (Epoch: 2025-07-01T18:26:27.672Z)
Latitude
55.42893°
Longitude
-19.42472°
Altitude
207.667 km
Speed
7.765 km/s
True Right ascension
11h 48m 59s
True Declination
55° 15' 17"
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
08:41:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
201.945 km
Perigee altitude
113.22 km
Semi-major axis
6,535.719 km
Eccentricity
0.00679
Inclination
97.303°
RAAN
187.9056°
Arg. of periapsis
204.0553°
True anomaly
211.94764°
Mean anomaly
212.361°
Eccentric anomaly
212.15403°
Mean motion
4.10774 °/min
Orbital period
87.64 mins
BSTAR
0.00024288
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Other satellites on launch #138 in the year 2025 (2025-06-26 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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