ELECTRON R/B, 100245

Orbit data source: Space-Track

ELECTRON R/B, 100245 is space debris in LEO originally from a launch on Thu, 06 Aug 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
100245, 2026-180C
Orbit
LEO
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)
2026-08-06 (1 month ago)
Launch vehicle
Unknown
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL, 8.0 m
Radar Cross Section
Large (>1 m²)

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

TLE from 1 day ago
0 ELECTRON R/B
1 A0245U 26180C   26253.92140733  .00697615  18651-3  12653-2 0  9992
2 A0245  41.9961 172.5908 0138940 129.8532 231.4642 15.85276000  5584
Epoch: 2026-09-10T22:06Z
TLE epoch observation values (Epoch: 2026-09-10T22:06:49.593Z)
Latitude
-0.00002°
Longitude
-149.06803°
Altitude
373.915 km
Speed
7.654 km/s
True Right ascension
11h 30m 21s
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
14:55:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
410.746 km
Perigee altitude
224.682 km
Semi-major axis
6,695.851 km
Eccentricity
0.01389
Inclination
41.9961°
RAAN
172.5908°
Arg. of periapsis
129.8532°
True anomaly
230.23223°
Mean anomaly
231.4642°
Eccentric anomaly
230.84688°
Mean motion
3.96127 °/min
Orbital period
90.88 mins
BSTAR
0.0012653
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Other satellites on launch #180 in the year 2026 (2026-08-06 UTC)

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