DECAYED

ELECTRON R/B, 58904 (Decayed)

Orbit data source: Public

ELECTRON R/B, 58904 was space debris originally from a launch on Wed, 31 Jan 2024 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

ELECTRON R/B details

Identifier	58904, 2024-022F
Orbit	Decayed
Last TLE update	Unknown
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)	2024-01-31 (11 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, Medium (>0.1 m² and < 1m²)

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Definitive object data

Latitude	Unknown
Longitude	Unknown
Altitude	Unknown
Speed	Unknown
True Right ascension	Unknown
True Declination	Unknown
Sunlit	N/A

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	Unknown
Perigee altitude	Unknown
Semi-major axis	Unknown
Eccentricity	Unknown
Inclination	Unknown
RAAN	Unknown
Arg. of periapsis	Unknown
True anomaly	Unknown
Mean anomaly	Unknown
Eccentric anomaly	Unknown
Mean motion	Unknown
BSTAR	Unknown
Orbital period	Unknown