ELECTRON R/B, 63305 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 63305 was space debris in LEO originally from a launch on Tue, 18 Mar 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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63305 intel report (Beta)
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Edit Public Description
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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 months ago
TLE from 6 months ago
0 ELECTRON R/B
1 63305U 25056F 25088.56110924 .28064676 21675-5 46598-3 0 9996
2 63305 97.9261 217.6347 0052197 204.2349 163.1487 16.41391216 1804Epoch: 2025-03-29T13:27Z
TLE epoch observation values (Epoch: 2025-03-29T13:27:59.838Z)
Latitude
7.40545°
Longitude
-172.5995°
Altitude
197.375 km
Speed
7.769 km/s
True Right ascension
14h 26m 24s
True Declination
7° 21' 28"
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
02:19:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
193.056 km
Perigee altitude
124.813 km
Semi-major axis
6,537.071 km
Eccentricity
0.00522
Inclination
97.9261°
RAAN
217.6347°
Arg. of periapsis
204.2349°
True anomaly
163.32102°
Mean anomaly
163.1487°
Eccentric anomaly
163.23497°
Mean motion
4.10647 °/min
Orbital period
87.67 mins
BSTAR
0.00046598
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Other satellites on launch #56 in the year 2025 (2025-03-18 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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