ELECTRON R/B, 64342
Orbit data source: Space-Track
ELECTRON R/B, 64342 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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64342 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
23 hours ago
Origin
Manufacturer
Rocket Lab
Mission
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
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & history
TLE from 23 hours ago
0 ELECTRON R/B
1 64342U 25125C 25199.42343095 .01520140 78632-5 14503-2 0 9999
2 64342 42.0125 201.9286 0112100 139.3790 332.9480 15.98902673 5778Epoch: 2025-07-18T10:09Z
TLE epoch observation values (Epoch: 2025-07-18T10:09:44.434Z)
Latitude
38.59431°
Longitude
-128.73734°
Altitude
213.216 km
Speed
7.823 km/s
True Right ascension
21h 20m 41s
True Declination
38° 24' 46"
Sunlit
Visualization orbit readout
Latitude
9.81319°
Longitude
-84.03769°
Altitude
202.644 km
Speed
7.826 km/s
Apparent Right ascension
03h 35m 40s
Apparent Declination
-35° 24' 19"
Sunlit
Visualization observer readout
Local Sidereal Time
21:39:57
Azimuth
119.128° SE
Elevation
-21.106°
Doppler factor
1
Orbital elements
Apogee altitude
354.272 km
Perigee altitude
205.004 km
Semi-major axis
6,657.775 km
Eccentricity
0.01121
Inclination
42.0125°
RAAN
201.9286°
Arg. of periapsis
139.379°
True anomaly
332.35641°
Mean anomaly
332.948°
Eccentric anomaly
332.65295°
Mean motion
3.9953 °/min
Orbital period
90.11 mins
BSTAR
0.0014503
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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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