ELECTRON KICK STAGE R/B, 59883 (Decayed)
Orbit data source: Space-Track
ELECTRON KICK STAGE R/B, 59883 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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59883 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
KICK STAGE, CURIE
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 3 months ago
TLE from 3 months ago
0 ELECTRON KICK STAGE R/B
1 59883U 24099C 25152.23561428 .06612873 25444-5 12470-2 0 9996
2 59883 97.4062 27.3853 0007856 221.2373 138.8329 16.32036096 57447Epoch: 2025-06-01T05:39Z
TLE epoch observation values (Epoch: 2025-06-01T05:39:17.073Z)
Latitude
-0.0001°
Longitude
52.59962°
Altitude
194.2 km
Speed
7.787 km/s
True Right ascension
01h 49m 32s
True Declination
0° 00' 00"
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
23:06:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
189.047 km
Perigee altitude
178.737 km
Semi-major axis
6,562.029 km
Eccentricity
0.00079
Inclination
97.4062°
RAAN
27.3853°
Arg. of periapsis
221.2373°
True anomaly
138.89211°
Mean anomaly
138.8329°
Eccentric anomaly
138.86251°
Mean motion
4.08306 °/min
Orbital period
88.17 mins
BSTAR
0.001247
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Other satellites on launch #99 in the year 2024 (2024-05-25 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 KICK STAGE 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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