ELECTRON R/B, 64342 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 64342 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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64342 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
1 week ago
Origin
Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
ELECTRON ST2, Unknown motor
Mass
250 kg wet, ~250 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, Unknown HBR
Radar Cross Section
2.827 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & history
TLE from 1 week ago
0 ELECTRON R/B
1 64342U 25125C 25205.05313362 .15764184 80645-5 81079-3 0 9993
2 64342 41.9997 165.3258 0033463 179.3550 231.5749 16.38356713 6683Epoch: 2025-07-24T01:16Z
TLE epoch observation values (Epoch: 2025-07-24T01:16:30.744Z)
Latitude
31.27504°
Longitude
-113.70253°
Altitude
184.456 km
Speed
7.793 km/s
True Right ascension
13h 49m 47s
True Declination
31° 06' 34"
Sunlit
Visualization orbit readout
No trajectory is available.
Visualization observer readout
No trajectory is available.
Orbital elements
Apogee altitude
194.311 km
Perigee altitude
150.471 km
Semi-major axis
6,550.528 km
Eccentricity
0.00335
Inclination
41.9997°
RAAN
165.3258°
Arg. of periapsis
179.355°
True anomaly
231.27527°
Mean anomaly
231.5749°
Eccentric anomaly
231.42501°
Mean motion
4.09382 °/min
Orbital period
87.94 mins
BSTAR
0.00081079
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Other satellites on launch #125 in the year 2025 (2025-06-11 UTC)
ELECTRON R/B Visibility
Observer location: undefined°, undefined°
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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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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Authenticating...
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