ELECTRON R/B, 69179

Orbit data source: Space-Track

ELECTRON R/B, 69179 is space debris in LEO originally from an American launch on Fri, 22 May 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
69179, 2026-112C
Orbit
LEO
Country
Flag of USUS
Related business
None
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2026-05-22 (2 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: 2 days ago

TLE from 2 days ago
0 ELECTRON R/B
1 69179U 26112C   26142.86980618  .00129570  85042-5  14133-3 0  9998
2 69179  44.9083 325.1175 0286327 260.0946  96.7520 15.61899702    75
Epoch: 2026-05-22T20:52Z
TLE epoch observation values (Epoch: 2026-05-22T20:52:31.253Z)
Latitude
-0.00002°
Longitude
131.4928°
Altitude
410.346 km
Speed
7.65 km/s
True Right ascension
21h 40m 28s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
04:03:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.434 km
Perigee altitude
190.208 km
Semi-major axis
6,761.958 km
Eccentricity
0.02863
Inclination
44.9083°
RAAN
325.1175°
Arg. of periapsis
260.0946°
True anomaly
99.99492°
Mean anomaly
96.752°
Eccentric anomaly
98.37504°
Mean motion
3.90332 °/min
Orbital period
92.23 mins
BSTAR
0.00014133
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Other satellites on launch #112 in the year 2026 (2026-05-22 UTC)

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