ELECTRON KICK STAGE R/B, 67230 (Decayed)
Orbit data source: Space-Track
ELECTRON KICK STAGE R/B, 67230 was space debris in LEO originally from a launch on Sun, 21 Dec 2025 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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Identifier
Orbit
Country
USRelated business
Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
KICK STAGE, CURIE
Mass
~42 kg wet, ~42 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Trunc Cone, 1.1 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 67230U 25307C 26016.09048044 .18058906 85429-5 45823-3 0 9994
2 67230 41.9939 323.2498 0017239 116.5376 243.7271 16.44299347 2486Epoch: 2026-01-16T02:10Z
TLE epoch observation values (Epoch: 2026-01-16T02:10:17.510Z)
Latitude
0.00001°
Longitude
175.1421°
Altitude
159.037 km
Speed
7.81 km/s
True Right ascension
21h 32m 59s
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
07:21:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
167.875 km
Perigee altitude
145.345 km
Semi-major axis
6,534.747 km
Eccentricity
0.00172
Inclination
41.9939°
RAAN
323.2498°
Arg. of periapsis
116.5376°
True anomaly
243.55013°
Mean anomaly
243.7271°
Eccentric anomaly
243.6386°
Mean motion
4.10866 °/min
Orbital period
87.62 mins
BSTAR
0.00045823
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Other satellites on launch #307 in the year 2025 (2025-12-21 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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