ELECTRON R/B (1), 66317 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B (1), 66317 was space debris in LEO originally from a launch on Wed, 05 Nov 2025 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
Orbit
Country
USRelated business
Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
KICK STAGE, CURIE
Mass
~42 kg wet, ~42 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Trunc Cone, 8.0 m
Radar Cross Section
0.760 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 months ago
TLE from 6 months ago
0 ELECTRON R/B (1)
1 66317U 25252B 25339.59423701 .10052791 84937-5 10112-2 0 9990
2 66317 41.9822 93.1396 0034449 86.6806 273.8008 16.34731361 4704Epoch: 2025-12-05T14:15Z
TLE epoch observation values (Epoch: 2025-12-05T14:15:42.077Z)
Latitude
-0.00002°
Longitude
164.58017°
Altitude
178.082 km
Speed
7.802 km/s
True Right ascension
06h 12m 33s
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
07:17:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
204.668 km
Perigee altitude
159.469 km
Semi-major axis
6,560.206 km
Eccentricity
0.00344
Inclination
41.9822°
RAAN
93.1396°
Arg. of periapsis
86.6806°
True anomaly
273.4068°
Mean anomaly
273.8008°
Eccentric anomaly
273.60381°
Mean motion
4.08476 °/min
Orbital period
88.13 mins
BSTAR
0.0010112
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Other satellites on launch #252 in the year 2025 (2025-11-05 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 (1) 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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