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.
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62087 intel report (Beta)
ELECTRON R/B details
Identifier | |
Orbit | Decayed |
Last TLE update | 3 weeks ago |
Origin | |
Manufacturer | Rocket Lab |
Mission | Decayed spacecraft |
Bus & Motor | KICK STAGE, CURIE |
Mass | ~50 kg wet, ~50 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 3 weeks 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 |
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Other satellites on launch #219 in the year 2024 (2024-11-25 UTC)
KINEIS-5C, 62081 |
KINEIS-5D, 62082 |
KINEIS-5E, 62083 |
KINEIS-5A, 62084 |
KINEIS-5B, 62085 |
ELECTRON KICK STAGE R/B, 62086 |
ELECTRON R/B, 62087 (Decayed) |
ELECTRON R/B Visibility forecast
Observer location: undefined°, undefined
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