ELECTRON R/B, 59589 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 59589 was space debris in LEO originally from a launch on Tue, 23 Apr 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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59589 intel report (Beta)
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ELECTRON R/B details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 6 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 6 months ago
0 ELECTRON R/B
1 59589U 24077C 24120.11832866 .25703934 18435-5 42399-3 0 9999
2 59589 97.3717 201.4229 0049442 202.9026 244.9909 16.41921092 828Epoch: 2024-04-29T02:50Z
Definitive object data (Epoch: 2024-04-29T02:50:23.596Z)
| Latitude | 82.22266° |
| Longitude | -129.09537° |
| Altitude | 188.031 km |
| Speed | 7.792 km/s |
| True Right ascension | 08h 44m 15s |
| True Declination | 82° 10' 21" |
| 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 | 189.814 km |
| Perigee | 125.187 km |
| Semi-major axis | 6,535.638 km |
| Eccentricity | 0.0049442 |
| Inclination | 97.3717° |
| RAAN | 201.4229° |
| Arg. of periapsis | 202.9026° |
| True anomaly | 244.4788° |
| Mean anomaly | 244.9909° |
| Eccentric anomaly | 244.73472° |
| Mean motion | 4.10782 °/min |
| BSTAR | 0.00042399 |
| Period | 87.64 mins |
No data available
No data available
Other satellites on launch #77 in the year 2024 (2024-04-23 UTC)
| NEONSAT-1, 59587 |
| ACS 3, 59588 |
| ELECTRON R/B, 59589 (Decayed) |
| ELECTRON KICK STAGE R/B, 59590 |
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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