ELECTRON R/B, 60354 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 60354 was space debris in LEO originally from a launch on Fri, 02 Aug 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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60354 intel report (Beta)
ELECTRON R/B details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 5 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 | Medium (>0.1 m² and <1 m²) |
Expand to show TLE details & history
TLE from 5 months ago
0 ELECTRON R/B
1 60354U 24137C 24227.06252620 .07493103 93388-5 13989-2 0 9990
2 60354 42.9539 69.9603 0070986 335.3226 163.4768 16.23819940 1794Epoch: 2024-08-14T01:30Z
Definitive object data (Epoch: 2024-08-14T01:30:02.263Z)
| Latitude | 26.63756° |
| Longitude | -127.91036° |
| Altitude | 254.083 km |
| Speed | 7.733 km/s |
| True Right ascension | 14h 30m 16s |
| True Declination | 26° 29' 22" |
| 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 | 258.01 km |
| Perigee altitude | 164.459 km |
| Semi-major axis | 6,589.372 km |
| Eccentricity | 0.0070986 |
| Inclination | 42.9539° |
| RAAN | 69.9603° |
| Arg. of periapsis | 335.3226° |
| True anomaly | 163.70619° |
| Mean anomaly | 163.4768° |
| Eccentric anomaly | 163.59169° |
| Mean motion | 4.05767 °/min |
| BSTAR | 0.0013989 |
| Orbital period | 88.72 mins |
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Other satellites on launch #137 in the year 2024 (2024-08-02 UTC)
| STRIX-4, 60352 |
| ELECTRON KICK STAGE R/B, 60353 |
| ELECTRON R/B, 60354 (Decayed) |
ELECTRON R/B Visibility forecast
Observer location: undefined°, undefined
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