DECAYED

ELECTRON R/B, 62087 (Decayed)

Orbit data source: Space-Track

ELECTRON R/B, 62087 was space debris in LEO originally from a launch on Mon, 25 Nov 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	62087, 2024-219G
Orbit	Decayed
Last TLE update	6 days ago
Origin	Rocket Lab (US)
Manufacturer	Rocket Lab
Mission	Decayed spacecraft
Bus & Motor	KICK STAGE, CURIE
Mass	~50 kg wet, ~50 kg dry
Launch date (UTC)	2024-11-25 (3 weeks 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 6 days ago

0 ELECTRON R/B
1 62087U 24219G   24342.74472910  .24207401  22635-5  35868-3 0  9996
2 62087  97.9193 143.6896 0043756 196.3431 294.5419 16.43612336  1989

Epoch: 2024-12-07T17:52Z

Definitive object data (Epoch: 2024-12-07T17:52:24.594Z)

Latitude	49.04446°
Longitude	-12.23624°
Altitude	152.287 km
Speed	7.827 km/s
True Right ascension	22h 11m 26s
True Declination	48° 51' 30"
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	181.616 km
Perigee altitude	124.46 km
Semi-major axis	6,531.175 km
Eccentricity	0.0043756
Inclination	97.9193°
RAAN	143.6896°
Arg. of periapsis	196.3431°
True anomaly	294.08476°
Mean anomaly	294.5419°
Eccentric anomaly	294.31343°
Mean motion	4.11203 °/min
BSTAR	0.00035868
Orbital period	87.55 mins