ELECTRON R/B, 67072 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 67072 was space debris in LEO originally from a launch on Sun, 14 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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67072 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, 8.0 m
Radar Cross Section
2.827 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 months ago
TLE from 6 months ago
0 ELECTRON R/B
1 67072U 25297A 25358.28094350 .10667753 20469-5 46079-3 0 9991
2 67072 97.4545 146.8421 0050860 206.0696 153.8040 16.35808035 1621Epoch: 2025-12-24T06:44Z
TLE epoch observation values (Epoch: 2025-12-24T06:44:33.518Z)
Latitude
0.00003°
Longitude
-47.35015°
Altitude
210.177 km
Speed
7.763 km/s
True Right ascension
09h 47m 22s
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
07:13:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
207.116 km
Perigee altitude
140.47 km
Semi-major axis
6,551.93 km
Eccentricity
0.00509
Inclination
97.4545°
RAAN
146.8421°
Arg. of periapsis
206.0696°
True anomaly
154.05982°
Mean anomaly
153.804°
Eccentric anomaly
153.93205°
Mean motion
4.09251 °/min
Orbital period
87.97 mins
BSTAR
0.00046079
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Other satellites on launch #297 in the year 2025 (2025-12-14 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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