ELECTRON KICK STAGE R/B, 55325 (Decayed)
Orbit data source: Space-Track
ELECTRON KICK STAGE R/B, 55325 was space debris in LEO originally from a launch on Tue, 24 Jan 2023 UTC launched from the Wallops Island (WLPIS). 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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55325 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: 5 months ago
TLE from 5 months ago
0 ELECTRON KICK STAGE R/B
1 55325U 23011B 25293.08929798 .05782817 70683-5 16385-2 0 9992
2 55325 40.4670 172.5269 0012608 266.5603 93.3800 16.26383006152770Epoch: 2025-10-20T02:08Z
TLE epoch observation values (Epoch: 2025-10-20T02:08:35.345Z)
Latitude
-0.00001°
Longitude
111.58301°
Altitude
202.25 km
Speed
7.787 km/s
True Right ascension
11h 30m 06s
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
17:58:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
213.047 km
Perigee altitude
196.447 km
Semi-major axis
6,582.884 km
Eccentricity
0.00126
Inclination
40.467°
RAAN
172.5269°
Arg. of periapsis
266.5603°
True anomaly
93.52421°
Mean anomaly
93.38°
Eccentric anomaly
93.45211°
Mean motion
4.06367 °/min
Orbital period
88.59 mins
BSTAR
0.0016385
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Other satellites on launch #11 in the year 2023 (2023-01-24 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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