ELECTRON KICK STAGE R/B, 56752 (Decayed)
Orbit data source: Space-Track
ELECTRON KICK STAGE R/B, 56752 was space debris in LEO originally from a launch on Fri, 26 May 2023 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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56752 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
KICK STAGE, CURIE
Mass
40 kg wet, ~40 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Trunc Cone, 0.7 m
Radar Cross Section
0.760 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 ELECTRON KICK STAGE R/B
1 56752U 23073A 25135.26296609 .03771493 -15301-5 16328-2 0 9998
2 56752 32.7022 214.2075 0005470 53.0862 307.0340 16.21439025110062Epoch: 2025-05-15T06:18Z
TLE epoch observation values (Epoch: 2025-05-15T06:18:40.270Z)
Latitude
-0.00003°
Longitude
-113.69584°
Altitude
212.091 km
Speed
7.783 km/s
True Right ascension
14h 16m 49s
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
21:24:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
223.017 km
Perigee altitude
215.799 km
Semi-major axis
6,597.545 km
Eccentricity
0.00055
Inclination
32.7022°
RAAN
214.2075°
Arg. of periapsis
53.0862°
True anomaly
306.98394°
Mean anomaly
307.034°
Eccentric anomaly
307.00897°
Mean motion
4.05014 °/min
Orbital period
88.89 mins
BSTAR
0.0016328
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Other satellites on launch #73 in the year 2023 (2023-05-26 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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