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.
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59966 intel report (Beta)
ELECTRON R/B details
Identifier | |
Orbit | Decayed |
Last TLE update | 8 months ago |
Origin | |
Manufacturer | Rocket Lab |
Mission | Decayed spacecraft |
Bus & Motor | ELECTRON ST2, Unknown motor |
Mass | 250 kg wet, ~250 kg dry |
Launch date (UTC) | |
Launch vehicle | Unknown |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Unknown |
Radar Cross Section | Large (>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)
Latitude | 43.89776° |
Longitude | -129.57075° |
Altitude | 168.957 km |
Speed | 7.799 km/s |
True Right ascension | 21h 03m 17s |
True Declination | 43° 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 altitude | 161.829 km |
Perigee altitude | 121.647 km |
Semi-major axis | 6,519.875 km |
Eccentricity | 0.0030815 |
Inclination | 97.476° |
RAAN | 323.0336° |
Arg. of periapsis | 193.7375° |
True anomaly | 210.53116° |
Mean anomaly | 210.7109° |
Eccentric anomaly | 210.62097° |
Mean motion | 4.12272 °/min |
BSTAR | 0.00032658 |
Orbital period | 87.32 mins |
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Other satellites on launch #108 in the year 2024 (2024-06-05 UTC)
PREFIRE-1, 59965 |
ELECTRON R/B, 59966 (Decayed) |
ELECTRON KICK STAGE R/B, 59967 |
ELECTRON R/B Visibility forecast
Observer location: undefined°, undefined
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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