DECAYED

ELECTRON R/B, 59966 (Decayed)

Orbit data source: Space-Track

ELECTRON R/B, 59966 was space debris in LEO originally from a launch on Wed, 05 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
59966, 2024-108B
Orbit
Decayed
Last TLE update8 months ago
Origin
Flag of USRocket Lab (US)
ManufacturerRocket Lab
MissionDecayed spacecraft
Bus & MotorELECTRON ST2, Unknown motor
Mass250 kg wet, ~250 kg dry
Launch date (UTC)
2024-06-05 (8 months ago)
Launch vehicleUnknown
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBRUnknown
Radar Cross SectionLarge (>1 m²)

Expand to show TLE details & history

TLE from 8 months ago
0 ELECTRON R/B
1 59966U 24108B   24170.49493666  .30482529  21787-5  32658-3 0  9991
2 59966  97.4760 323.0336 0030815 193.7375 210.7109 16.47875042  2110
Epoch: 2024-06-18T11:52Z
Definitive object data (Epoch: 2024-06-18T11:52:42.527Z)
Latitude43.89776°
Longitude-129.57075°
Altitude168.957 km
Speed7.799 km/s
True Right ascension21h 03m 17s
True Declination43° 42' 38"
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 altitude161.829 km
Perigee altitude121.647 km
Semi-major axis6,519.875 km
Eccentricity0.0030815
Inclination97.476°
RAAN323.0336°
Arg. of periapsis193.7375°
True anomaly210.53116°
Mean anomaly210.7109°
Eccentric anomaly210.62097°
Mean motion4.12272 °/min
BSTAR0.00032658
Orbital period87.32 mins
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Other satellites on launch #108 in the year 2024 (2024-06-05 UTC)

ELECTRON R/B Visibility forecast

Observer location: undefined°, undefined

This satellite is decayed
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