ELECTRON R/B, 68410 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 68410 was space debris in LEO 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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68410 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
ELECTRON ST2, Unknown motor
Mass
250 kg wet, ~250 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 1 week ago
TLE from 1 week ago
0 ELECTRON R/B
1 68410U 26065C 26093.36915547 .13281109 16595-5 48423-3 0 9998
2 68410 97.3609 336.1707 0069854 198.0172 161.8648 16.33068968 882Epoch: 2026-04-03T08:51Z
TLE epoch observation values (Epoch: 2026-04-03T08:51:35.032Z)
Latitude
-0.00003°
Longitude
11.57046°
Altitude
231.154 km
Speed
7.742 km/s
True Right ascension
22h 24m 40s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
19:09:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
226.939 km
Perigee altitude
135.301 km
Semi-major axis
6,559.257 km
Eccentricity
0.00699
Inclination
97.3609°
RAAN
336.1707°
Arg. of periapsis
198.0172°
True anomaly
162.1119°
Mean anomaly
161.8648°
Eccentric anomaly
161.98856°
Mean motion
4.08565 °/min
Orbital period
88.11 mins
BSTAR
0.00048423
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Other satellites on launch #65 in the year 2026 (2026-03-28 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ELECTRON R/B Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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