ELECTRON R/B, 101258

Orbit data source: Space-Track

ELECTRON R/B, 101258 is space debris in LEO originally from an American launch on Mon, 02 Nov 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
101258, 2026-247B
Orbit
LEO
Country
Flag of USUS
Related business
None
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2026-11-02 (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: 11 hours ago

TLE from 11 hours ago
0 ELECTRON R/B
1 A1258U 26247B   26307.94123979  .00247126  22155-4  83762-3 0  9999
2 A1258  42.0376 219.3094 0259466 250.2758 106.9930 15.52383788   197
Epoch: 2026-11-03T22:35Z
TLE epoch observation values (Epoch: 2026-11-03T22:35:23.117Z)
Latitude
-0.00003°
Longitude
-162.73364°
Altitude
465.026 km
Speed
7.605 km/s
True Right ascension
14h 37m 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
05:55:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.078 km
Perigee altitude
235.721 km
Semi-major axis
6,790.036 km
Eccentricity
0.02595
Inclination
42.0376°
RAAN
219.3094°
Arg. of periapsis
250.2758°
True anomaly
109.80861°
Mean anomaly
106.993°
Eccentric anomaly
108.4036°
Mean motion
3.87914 °/min
Orbital period
92.8 mins
BSTAR
0.00083762
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Other satellites on launch #247 in the year 2026 (2026-11-02 UTC)

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