ELECTRON R/B, 64232 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 64232 was space debris in LEO originally from a launch on Mon, 02 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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64232 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
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 & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 ELECTRON R/B
1 64232U 25118C 25162.61083509 .11505920 10807-4 34541-3 0 9995
2 64232 58.9851 180.7417 0068432 278.6129 185.4289 16.34335593 1360Epoch: 2025-06-11T14:39Z
TLE epoch observation values (Epoch: 2025-06-11T14:39:36.151Z)
Latitude
56.41749°
Longitude
176.44699°
Altitude
233.442 km
Speed
7.747 km/s
True Right ascension
19h 46m 09s
True Declination
56° 14' 46"
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
08:33:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
225.115 km
Perigee altitude
135.355 km
Semi-major axis
6,558.372 km
Eccentricity
0.00684
Inclination
58.9851°
RAAN
180.7417°
Arg. of periapsis
278.6129°
True anomaly
185.35534°
Mean anomaly
185.4289°
Eccentric anomaly
185.39206°
Mean motion
4.08648 °/min
Orbital period
88.1 mins
BSTAR
0.00034541
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Other satellites on launch #118 in the year 2025 (2025-06-02 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 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
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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