ELECTRON KICK STAGE R/B, 67224 (Decayed)
Orbit data source: Space-Track
ELECTRON KICK STAGE R/B, 67224 was space debris in LEO originally from a launch on Thu, 18 Dec 2025 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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Identifier
Orbit
Country
USRelated business
Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
ELECTRON ST2, Unknown motor
Mass
250 kg wet, ~250 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 8.0 m
Radar Cross Section
2.827 m²
Expand to show TLE details & historyLast TLE update: 3 months ago
TLE from 3 months ago
0 ELECTRON KICK STAGE R/B
1 67224U 25305F 26006.95949992 .16622258 10931-4 21249-3 0 9997
2 67224 44.9837 203.5690 0020541 49.5317 310.7398 16.47594125 3147Epoch: 2026-01-06T23:01Z
TLE epoch observation values (Epoch: 2026-01-06T23:01:40.793Z)
Latitude
-0.00002°
Longitude
111.61419°
Altitude
136.947 km
Speed
7.831 km/s
True Right ascension
13h 34m 16s
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
03:55:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
160.778 km
Perigee altitude
133.97 km
Semi-major axis
6,525.511 km
Eccentricity
0.00205
Inclination
44.9837°
RAAN
203.569°
Arg. of periapsis
49.5317°
True anomaly
310.56116°
Mean anomaly
310.7398°
Eccentric anomaly
310.65051°
Mean motion
4.11738 °/min
Orbital period
87.43 mins
BSTAR
0.00021249
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Other satellites on launch #305 in the year 2025 (2025-12-18 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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