DECAYED

ELECTRON R/B, 59589 (Decayed)

Orbit data source: Space-Track

ELECTRON R/B, 59589 was space debris in LEO originally from a launch on Tue, 23 Apr 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	59589, 2024-077C
Orbit	Decayed
Last TLE update	7 months 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)	2024-04-23 (7 months ago)
Launch vehicle	Unknown
Launch site	Rocket Lab Launch Complex (RLLC)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history

TLE from 7 months ago

0 ELECTRON R/B
1 59589U 24077C   24120.11832866  .25703934  18435-5  42399-3 0  9999
2 59589  97.3717 201.4229 0049442 202.9026 244.9909 16.41921092   828

Epoch: 2024-04-29T02:50Z

Definitive object data (Epoch: 2024-04-29T02:50:23.596Z)

Latitude	82.22266°
Longitude	-129.09537°
Altitude	188.031 km
Speed	7.792 km/s
True Right ascension	08h 44m 15s
True Declination	82° 10' 21"
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	189.814 km
Perigee altitude	125.187 km
Semi-major axis	6,535.638 km
Eccentricity	0.0049442
Inclination	97.3717°
RAAN	201.4229°
Arg. of periapsis	202.9026°
True anomaly	244.4788°
Mean anomaly	244.9909°
Eccentric anomaly	244.73472°
Mean motion	4.10782 °/min
BSTAR	0.00042399
Orbital period	87.64 mins