ELECTRON DEB, 64343
Orbit data source: Space-Track
ELECTRON DEB, 64343 is 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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64343 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
2 months ago
Origin
RLABN (US)Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & history
TLE from 2 months ago
0 ELECTRON DEB
1 64343U 25125D 25163.14389056 .19862338 62886-5 35037-1 0 9992
2 64343 42.0238 64.6207 0204325 234.1039 277.4123 15.73018143 70Epoch: 2025-06-12T03:27Z
TLE epoch observation values (Epoch: 2025-06-12T03:27:12.144Z)
Latitude
20.1205°
Longitude
-91.74008°
Altitude
334.549 km
Speed
7.72 km/s
True Right ascension
14h 43m 06s
True Declination
20° 00' 10"
Sunlit
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.
Orbital elements
Apogee altitude
489.95 km
Perigee altitude
214.906 km
Semi-major axis
6,730.565 km
Eccentricity
0.02043
Inclination
42.0238°
RAAN
64.6207°
Arg. of periapsis
234.1039°
True anomaly
275.08344°
Mean anomaly
277.4123°
Eccentric anomaly
276.24856°
Mean motion
3.93066 °/min
Orbital period
91.59 mins
BSTAR
0.035037
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Other satellites on launch #125 in the year 2025 (2025-06-11 UTC)
ELECTRON DEB 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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