DECAYED

ELECTRON R/B, 60080 (Decayed)

Orbit data source: Space-Track

ELECTRON R/B, 60080 was space debris in LEO originally from a launch on Thu, 20 Jun 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	60080, 2024-114B
Orbit	Decayed
Last TLE update	5 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)	2024-06-20 (6 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 5 months ago

0 ELECTRON R/B
1 60080U 24114B   24191.33362157  .03351378  28213-5  10000-3 0  9998
2 60080  97.9887 210.0944 0037508 162.4915 323.4653 16.40261238  2916

Epoch: 2024-07-09T08:00Z

Definitive object data (Epoch: 2024-07-09T08:00:24.903Z)

Latitude	53.64462°
Longitude	-6.83655°
Altitude	154.298 km
Speed	7.831 km/s
True Right ascension	02h 44m 05s
True Declination	53° 27' 54"
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	186.473 km
Perigee altitude	137.412 km
Semi-major axis	6,540.079 km
Eccentricity	0.0037508
Inclination	97.9887°
RAAN	210.0944°
Arg. of periapsis	162.4915°
True anomaly	323.20846°
Mean anomaly	323.4653°
Eccentric anomaly	323.33698°
Mean motion	4.10363 °/min
BSTAR	0.0001
Orbital period	87.73 mins