ELECTRON R/B, 68410

Orbit data source: Space-Track

ELECTRON R/B, 68410 is space debris in SSO originally from a launch on Sat, 28 Mar 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
68410, 2026-065C
Orbit
SSO
Country
Flag of ESAESA
Related business
Manufacturer
Rocket Lab
Mission
Spacecraft
Bus & Motor
ELECTRON ST2, Unknown motor
Mass
250 kg wet, ~250 kg dry
Launch date (UTC)
2026-03-28 (4 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 68410U 26065C   26088.74355105  .00479178  22642-5  25022-3 0  9993
2 68410  97.3942 331.0573 0228083 205.9229 153.0475 15.83047135   157
Epoch: 2026-03-29T17:50Z
TLE epoch observation values (Epoch: 2026-03-29T17:50:42.810Z)
Latitude
0.00003°
Longitude
-123.76614°
Altitude
461.949 km
Speed
7.557 km/s
True Right ascension
22h 04m 13s
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
01:43:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.452 km
Perigee altitude
165.965 km
Semi-major axis
6,696.846 km
Eccentricity
0.02281
Inclination
97.3942°
RAAN
331.0573°
Arg. of periapsis
205.9229°
True anomaly
154.20267°
Mean anomaly
153.0475°
Eccentric anomaly
153.62799°
Mean motion
3.96039 °/min
Orbital period
90.9 mins
BSTAR
0.00025022
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Other satellites on launch #65 in the year 2026 (2026-03-28 UTC)

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