ELECTRON R/B, 59882 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 59882 was space debris in LEO originally from a launch on Sat, 25 May 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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59882 intel report (Beta)
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ELECTRON R/B details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 4 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 4 months ago
0 ELECTRON R/B
1 59882U 24099B 24162.35253499 .26591496 21862-5 37978-3 0 9994
2 59882 97.4512 21.7750 0027981 183.1273 235.1261 16.46282928 2545Epoch: 2024-06-10T08:27Z
Definitive object data (Epoch: 2024-06-10T08:27:39.023Z)
| Latitude | 57.33377° |
| Longitude | -16.02835° |
| Altitude | 169.334 km |
| Speed | 7.804 km/s |
| True Right ascension | 00h 40m 17s |
| True Declination | 57° 09' 48" |
| 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 | 164.199 km |
| Perigee | 127.689 km |
| Semi-major axis | 6,524.081 km |
| Eccentricity | 0.0027981 |
| Inclination | 97.4512° |
| RAAN | 21.775° |
| Arg. of periapsis | 183.1273° |
| True anomaly | 234.86357° |
| Mean anomaly | 235.1261° |
| Eccentric anomaly | 234.99478° |
| Mean motion | 4.11874 °/min |
| BSTAR | 0.00037978 |
| Period | 87.41 mins |
No data available
No data available
Other satellites on launch #99 in the year 2024 (2024-05-25 UTC)
| PREFIRE-2, 59881 |
| ELECTRON R/B, 59882 (Decayed) |
| ELECTRON KICK STAGE R/B, 59883 |
ELECTRON R/B Visibility forecast
Observer location: 39.9160978°, -105.1181434
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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