ELECTRON DEB, 64343 (Decayed)
Orbit data source: Space-Track
ELECTRON DEB, 64343 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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64343 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 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 orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
23:48:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
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)
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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 DEB 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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