ELECTRON R/B, 68292 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 68292 was space debris in LEO originally from a launch on Fri, 20 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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68292 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 3 months ago
TLE from 3 months ago
0 ELECTRON R/B
1 68292U 26056B 26090.67010522 .18717014 12617-4 26663-3 0 9992
2 68292 50.2448 348.6579 0054105 288.0944 71.4175 16.41668461 1733Epoch: 2026-03-31T16:04Z
TLE epoch observation values (Epoch: 2026-03-31T16:04:57.091Z)
Latitude
-0.00002°
Longitude
-81.62395°
Altitude
150.876 km
Speed
7.824 km/s
True Right ascension
23h 14m 37s
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
07:23:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
197.522 km
Perigee altitude
126.75 km
Semi-major axis
6,540.273 km
Eccentricity
0.00541
Inclination
50.2448°
RAAN
348.6579°
Arg. of periapsis
288.0944°
True anomaly
72.00643°
Mean anomaly
71.4175°
Eccentric anomaly
71.71184°
Mean motion
4.10345 °/min
Orbital period
87.73 mins
BSTAR
0.00026663
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Other satellites on launch #56 in the year 2026 (2026-03-20 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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