ELECTRON R/B, 67558 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 67558 was space debris in LEO originally from a launch on Thu, 22 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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67558 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: 4 months ago
TLE from 4 months ago
0 ELECTRON R/B
1 67558U 26015C 26052.88646332 .22895390 -21477-5 29551-3 0 9990
2 67558 88.9324 279.2183 0066057 153.0615 207.4152 16.40773153 4646Epoch: 2026-02-21T21:16Z
TLE epoch observation values (Epoch: 2026-02-21T21:16:30.430Z)
Latitude
-0.00002°
Longitude
168.28889°
Altitude
205.539 km
Speed
7.76 km/s
True Right ascension
18h 36m 52s
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
07:24:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
203.581 km
Perigee altitude
117.198 km
Semi-major axis
6,538.526 km
Eccentricity
0.00661
Inclination
88.9324°
RAAN
279.2183°
Arg. of periapsis
153.0615°
True anomaly
207.06921°
Mean anomaly
207.4152°
Eccentric anomaly
207.24195°
Mean motion
4.1051 °/min
Orbital period
87.7 mins
BSTAR
0.00029551
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Other satellites on launch #15 in the year 2026 (2026-01-22 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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