DECAYED

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.

Not visible in the next 10 days
Identifier
63305, 2025-056F
Orbit
Decayed
Last TLE update
1 month ago
Origin
Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
ELECTRON ST2, Unknown motor
Mass
250 kg wet, ~250 kg dry
Launch date (UTC)
2025-03-18 (2 months ago)
Launch vehicle
Unknown
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, Unknown HBR
Radar Cross Section
2.827 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 month 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  1804
Epoch: 2025-03-29T13:27Z
Definitive object data (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
Object was in full shadow at TLE epoch
Visualization observer readout
Visualization observer readout
Orbital elements
Apogee altitude
193.056 km
Perigee altitude
124.813 km
Semi-major axis
6,537.071 km
Eccentricity
0.0052197
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
BSTAR
0.00046598
Orbital period
87.67 mins
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ELECTRON R/B Visibility forecast

Observer location: undefined°, undefined°

This satellite is decayed
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