ELECTRON R/B, 67229 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 67229 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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67229 intel report (Beta)
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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, 1.1 m
Radar Cross Section
2.827 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 months ago
TLE from 5 months ago
0 ELECTRON R/B
1 67229U 25307B 26023.74443348 .11096615 81342-5 12182-2 0 9991
2 67229 41.9806 276.6317 0032361 133.7549 226.6011 16.34241042 5285Epoch: 2026-01-23T17:51Z
TLE epoch observation values (Epoch: 2026-01-23T17:51:59.052Z)
Latitude
-0.00003°
Longitude
-114.44323°
Altitude
195.431 km
Speed
7.782 km/s
True Right ascension
18h 26m 31s
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
08:46:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
204.614 km
Perigee altitude
162.146 km
Semi-major axis
6,561.517 km
Eccentricity
0.00324
Inclination
41.9806°
RAAN
276.6317°
Arg. of periapsis
133.7549°
True anomaly
226.33241°
Mean anomaly
226.6011°
Eccentric anomaly
226.46668°
Mean motion
4.08354 °/min
Orbital period
88.16 mins
BSTAR
0.0012182
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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 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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