ELECTRON R/B, 67615

Orbit data source: Space-Track

ELECTRON R/B, 67615 is space debris in SSO 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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Identifier
67615, 2026-019B
Orbit
SSO
Country
Flag of UnknownUnknown / SKOR
Related business
Manufacturer
Rocket Lab
Mission
Spacecraft
Bus & Motor
ELECTRON ST2, Unknown motor
Mass
250 kg wet, ~250 kg dry
Launch date (UTC)
2026-01-30 (3 days ago)
Launch vehicle
Unknown
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 ELECTRON R/B
1 67615U 26019B   26031.74548725  .00250226  22837-5  25521-3 0  9999
2 67615  97.4470 156.8497 0259152 220.4311 137.7440 15.69235212   265
Epoch: 2026-01-31T17:53Z
TLE epoch observation values (Epoch: 2026-01-31T17:53:30.098Z)
Latitude
-0.00001°
Longitude
117.50923°
Altitude
495.526 km
Speed
7.542 km/s
True Right ascension
10h 27m 23s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
07:33:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
532.553 km
Perigee altitude
183.417 km
Semi-major axis
6,736.122 km
Eccentricity
0.02592
Inclination
97.447°
RAAN
156.8497°
Arg. of periapsis
220.4311°
True anomaly
139.69376°
Mean anomaly
137.744°
Eccentric anomaly
138.72353°
Mean motion
3.9258 °/min
Orbital period
91.7 mins
BSTAR
0.00025521
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Other satellites on launch #19 in the year 2026 (2026-01-30 UTC)

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