ELECTRON R/B, 101147

Orbit data source: Space-Track

ELECTRON R/B, 101147 is space debris in SSO originally from a launch on Fri, 23 Oct 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
101147, 2026-239D
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Rocket Lab
Mission
Spacecraft
Bus & Motor
ELECTRON ST2, Unknown motor
Mass
250 kg wet, ~250 kg dry
Launch date (UTC)
2026-10-23 (2 days ago)
Launch vehicle
Unknown
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL, 1.2 m
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 A1147U 26239D   26297.27995306  .02374468  21458-5  11902-2 0  9996
2 A1147  97.4265 146.0623 0244830 207.0724 151.7603 15.79729557   159
Epoch: 2026-10-24T06:43Z
TLE epoch observation values (Epoch: 2026-10-24T06:43:07.944Z)
Latitude
-0.00007°
Longitude
12.59079°
Altitude
479.997 km
Speed
7.542 km/s
True Right ascension
09h 44m 14s
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
05:18:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
492.28 km
Perigee altitude
163.902 km
Semi-major axis
6,706.228 km
Eccentricity
0.02448
Inclination
97.4265°
RAAN
146.0623°
Arg. of periapsis
207.0724°
True anomaly
153.05278°
Mean anomaly
151.7603°
Eccentric anomaly
152.40998°
Mean motion
3.95208 °/min
Orbital period
91.09 mins
BSTAR
0.0011902
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Other satellites on launch #239 in the year 2026 (2026-10-23 UTC)

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