ELECTRON R/B, 65972

Orbit data source: Space-Track

ELECTRON R/B, 65972 is space debris in LEO originally from a launch on Tue, 14 Oct 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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Identifier
65972, 2025-229B
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Rocket Lab
Mission
Operational spacecraft
Bus & Motor
ELECTRON ST2, Unknown motor
Mass
250 kg wet, ~250 kg dry
Launch date (UTC)
2025-10-14 (1 month ago)
Launch vehicle
Unknown
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 8.0 m
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 ELECTRON R/B
1 65972U 25229B   25312.05680473  .00007550  00000-0  57453-3 0  9999
2 65972  41.9280  71.4275 0038585  44.3366 316.0539 15.01793365  3679
Epoch: 2025-11-08T01:21Z
TLE epoch observation values (Epoch: 2025-11-08T01:21:47.928Z)
Latitude
-0.00001°
Longitude
3.4859°
Altitude
541.801 km
Speed
7.604 km/s
True Right ascension
04h 45m 42s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
04:07:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.251 km
Perigee altitude
536.683 km
Semi-major axis
6,941.604 km
Eccentricity
0.00386
Inclination
41.928°
RAAN
71.4275°
Arg. of periapsis
44.3366°
True anomaly
315.74599°
Mean anomaly
316.0539°
Eccentric anomaly
315.90005°
Mean motion
3.75278 °/min
Orbital period
95.93 mins
BSTAR
0.00057453
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Other satellites on launch #229 in the year 2025 (2025-10-14 UTC)

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