ELECTRON R/B, 67615 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 67615 was space debris in LEO originally from a launch on Fri, 30 Jan 2026 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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67615 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
Unknown shape, 8.0 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 ELECTRON R/B
1 67615U 26019B 26042.49253174 .15754726 19625-5 86016-3 0 9991
2 67615 97.4091 168.6564 0041350 200.0421 159.9255 16.36375123 1975Epoch: 2026-02-11T11:49Z
TLE epoch observation values (Epoch: 2026-02-11T11:49:14.742Z)
Latitude
-0.00002°
Longitude
-150.21289°
Altitude
204.181 km
Speed
7.769 km/s
True Right ascension
11h 14m 37s
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
11:50:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
199.362 km
Perigee altitude
145.19 km
Semi-major axis
6,550.413 km
Eccentricity
0.00414
Inclination
97.4091°
RAAN
168.6564°
Arg. of periapsis
200.0421°
True anomaly
160.08735°
Mean anomaly
159.9255°
Eccentric anomaly
160.00651°
Mean motion
4.09393 °/min
Orbital period
87.94 mins
BSTAR
0.00086016
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Other satellites on launch #19 in the year 2026 (2026-01-30 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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