ELECTRON R/B, 67223
Orbit data source: Space-Track
ELECTRON R/B, 67223 is 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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67223 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Rocket Lab
Mission
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
Trunc Cone, 8.0 m
Radar Cross Section
0.760 m²
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ELECTRON R/B
1 67223U 25305E 26092.86443249 .15252796 10618-4 87668-3 0 9999
2 67223 44.9587 68.6394 0006302 60.8918 299.2638 16.41630620 16586Epoch: 2026-04-02T20:44Z
TLE epoch observation values (Epoch: 2026-04-02T20:44:46.967Z)
Latitude
-0.00001°
Longitude
-73.7631°
Altitude
159.45 km
Speed
7.814 km/s
True Right ascension
04h 34m 33s
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
03:55:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
167.286 km
Perigee altitude
159.041 km
Semi-major axis
6,541.301 km
Eccentricity
0.00063
Inclination
44.9587°
RAAN
68.6394°
Arg. of periapsis
60.8918°
True anomaly
299.20078°
Mean anomaly
299.2638°
Eccentric anomaly
299.23229°
Mean motion
4.10248 °/min
Orbital period
87.75 mins
BSTAR
0.00087668
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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 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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| ELECTRON R/B is likely not visible in the next few days. |
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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