ELECTRON R/B, 61794 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 61794 was space debris in LEO originally from a launch on Tue, 05 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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61794 intel report (Beta)
ELECTRON R/B details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 1 month 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 1 month ago
0 ELECTRON R/B
1 61794U 24201C 24328.91290801 .28009577 23251-5 54894-3 0 9994
2 61794 97.8628 235.6162 0037199 160.1510 263.3626 16.42832349 2896Epoch: 2024-11-23T21:54Z
Definitive object data (Epoch: 2024-11-23T21:54:35.252Z)
| Latitude | 62.15056° |
| Longitude | -171.45272° |
| Altitude | 171.88 km |
| Speed | 7.807 km/s |
| True Right ascension | 14h 42m 12s |
| True Declination | 61° 59' 44" |
| 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 | 179.407 km |
| Perigee altitude | 130.801 km |
| Semi-major axis | 6,533.241 km |
| Eccentricity | 0.0037199 |
| Inclination | 97.8628° |
| RAAN | 235.6162° |
| Arg. of periapsis | 160.151° |
| True anomaly | 262.93942° |
| Mean anomaly | 263.3626° |
| Eccentric anomaly | 263.15099° |
| Mean motion | 4.11008 °/min |
| BSTAR | 0.00054894 |
| Orbital period | 87.59 mins |
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Other satellites on launch #201 in the year 2024 (2024-11-05 UTC)
| ELECTRON KICK STAGE R/B, 61792 (Decayed) |
| PROTOSAT-1, 61793 |
| ELECTRON R/B, 61794 (Decayed) |
ELECTRON R/B Visibility forecast
Observer location: undefined°, undefined
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