ELECTRON R/B (2), 68801 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B (2), 68801 was space debris in LEO originally from a launch on Thu, 23 Apr 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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68801 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
KICK STAGE, CURIE
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 8.0 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 ELECTRON R/B (2)
1 68801U 26088K 26132.69883670 .12520094 21931-5 24337-3 0 9994
2 68801 97.4647 285.2889 0040705 216.2899 143.5640 16.42313001 3105Epoch: 2026-05-12T16:46Z
TLE epoch observation values (Epoch: 2026-05-12T16:46:19.490Z)
Latitude
-0.00005°
Longitude
163.23823°
Altitude
184.362 km
Speed
7.783 km/s
True Right ascension
19h 01m 09s
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
07:19:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
183.063 km
Perigee altitude
129.865 km
Semi-major axis
6,534.601 km
Eccentricity
0.00407
Inclination
97.4647°
RAAN
285.2889°
Arg. of periapsis
216.2899°
True anomaly
143.8399°
Mean anomaly
143.564°
Eccentric anomaly
143.70206°
Mean motion
4.1088 °/min
Orbital period
87.62 mins
BSTAR
0.00024337
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Other satellites on launch #88 in the year 2026 (2026-04-23 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 (2) 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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