ELECTRON R/B, 59966 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 59966 was space debris in LEO originally from a launch on Wed, 05 Jun 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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59966 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
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
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 ELECTRON R/B
1 59966U 24108B 24170.49493666 .30482529 21787-5 32658-3 0 9991
2 59966 97.4760 323.0336 0030815 193.7375 210.7109 16.47875042 2110Epoch: 2024-06-18T11:52Z
TLE epoch observation values (Epoch: 2024-06-18T11:52:42.527Z)
Latitude
43.89776°
Longitude
-129.57075°
Altitude
168.957 km
Speed
7.799 km/s
True Right ascension
21h 03m 17s
True Declination
43° 42' 38"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
19:41:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
161.829 km
Perigee altitude
121.647 km
Semi-major axis
6,519.875 km
Eccentricity
0.00308
Inclination
97.476°
RAAN
323.0336°
Arg. of periapsis
193.7375°
True anomaly
210.53116°
Mean anomaly
210.7109°
Eccentric anomaly
210.62097°
Mean motion
4.12272 °/min
Orbital period
87.32 mins
BSTAR
0.00032658
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Other satellites on launch #108 in the year 2024 (2024-06-05 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ELECTRON R/B Visibility
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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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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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