ELECTRON KICK STAGE R/B, 59967 (Decayed)
Orbit data source: Space-Track
ELECTRON KICK STAGE R/B, 59967 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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59967 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: 5 months ago
TLE from 5 months ago
0 ELECTRON KICK STAGE R/B
1 59967U 24108C 25093.85518764 .12035746 25498-5 62710-3 0 9994
2 59967 97.4182 258.9606 0012373 288.7956 71.2002 16.41439182 46759Epoch: 2025-04-03T20:31Z
TLE epoch observation values (Epoch: 2025-04-03T20:31:28.212Z)
Latitude
0.00005°
Longitude
118.671°
Altitude
162.63 km
Speed
7.81 km/s
True Right ascension
17h 15m 50s
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
12:19:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
166.872 km
Perigee altitude
150.695 km
Semi-major axis
6,536.92 km
Eccentricity
0.00124
Inclination
97.4182°
RAAN
258.9606°
Arg. of periapsis
288.7956°
True anomaly
71.33449°
Mean anomaly
71.2002°
Eccentric anomaly
71.26734°
Mean motion
4.10661 °/min
Orbital period
87.66 mins
BSTAR
0.0006271
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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 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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