ELECTRON R/B, 65118 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 65118 was space debris in LEO originally from a launch on Tue, 05 Aug 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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65118 intel report (Beta)
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Edit Public Description
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
Cyl, 8.0 m
Radar Cross Section
2.827 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 months ago
TLE from 3 months ago
0 ELECTRON R/B
1 65118U 25169C 25248.05570646 .06901951 81467-5 13887-2 0 9999
2 65118 42.0018 120.3377 0051070 124.0548 236.5186 16.26280077 4877Epoch: 2025-09-05T01:20Z
TLE epoch observation values (Epoch: 2025-09-05T01:20:13.038Z)
Latitude
-0.00003°
Longitude
115.87396°
Altitude
220.862 km
Speed
7.765 km/s
True Right ascension
08h 01m 21s
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
21:32:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
238.377 km
Perigee altitude
171.139 km
Semi-major axis
6,582.895 km
Eccentricity
0.00511
Inclination
42.0018°
RAAN
120.3377°
Arg. of periapsis
124.0548°
True anomaly
236.03221°
Mean anomaly
236.5186°
Eccentric anomaly
236.27523°
Mean motion
4.06366 °/min
Orbital period
88.59 mins
BSTAR
0.0013887
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Other satellites on launch #169 in the year 2025 (2025-08-05 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 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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