DECAYED

ELECTRON R/B, 62933 (Decayed)

Orbit data source: Space-Track

ELECTRON R/B, 62933 was space debris in LEO originally from a launch on Sat, 08 Feb 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	62933, 2025-028F
Orbit	Decayed
Last TLE update	3 weeks ago
Origin	Rocket Lab (US)
Manufacturer	Rocket Lab
Mission	Decayed spacecraft
Bus & Motor	ELECTRON ST2, Unknown motor
Mass	250 kg wet, ~250 kg dry
Launch date (UTC)	2025-02-08 (1 month ago)
Launch vehicle	Unknown
Launch site	Rocket Lab Launch Complex (RLLC)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	Large (>1 m²)

Expand to show TLE details & history

TLE from 3 weeks ago

0 ELECTRON R/B
1 62933U 25028F   25051.88207345  .13714693  21991-5  27058-3 0  9996
2 62933  97.9272 109.5562 0054540 197.5517 275.2945 16.39810484  1876

Epoch: 2025-02-20T21:10Z

Definitive object data (Epoch: 2025-02-20T21:10:11.146Z)

Latitude	66.56626°
Longitude	-160.41429°
Altitude	174.739 km
Speed	7.81 km/s
True Right ascension	20h 32m 44s
True Declination	66° 25' 45"
Sunlit	Object was in daylight at TLE epoch

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Orbital elements

Apogee altitude	198.815 km
Perigee altitude	127.463 km
Semi-major axis	6,541.276 km
Eccentricity	0.005454
Inclination	97.9272°
RAAN	109.5562°
Arg. of periapsis	197.5517°
True anomaly	274.6718°
Mean anomaly	275.2945°
Eccentric anomaly	274.98319°
Mean motion	4.10251 °/min
BSTAR	0.00027058
Orbital period	87.75 mins