ELECTRON R/B, 65118
Orbit data source: Space-Track
ELECTRON R/B, 65118 is 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
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
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 ELECTRON R/B
1 65118U 25169C 25241.26470610 .01390276 78709-5 16989-2 0 9993
2 65118 42.0156 163.9490 0145540 68.9718 292.6638 15.89538446 3788Epoch: 2025-08-29T06:21Z
TLE epoch observation values (Epoch: 2025-08-29T06:21:10.607Z)
Latitude
-0.00003°
Longitude
90.93893°
Altitude
266.982 km
Speed
7.77 km/s
True Right ascension
10h 55m 47s
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
14:11:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
403.02 km
Perigee altitude
208.466 km
Semi-major axis
6,683.88 km
Eccentricity
0.01455
Inclination
42.0156°
RAAN
163.949°
Arg. of periapsis
68.9718°
True anomaly
291.11414°
Mean anomaly
292.6638°
Eccentric anomaly
291.89004°
Mean motion
3.97192 °/min
Orbital period
90.64 mins
BSTAR
0.0016989
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Other satellites on launch #169 in the year 2025 (2025-08-05 UTC)
ELECTRON R/B Visibility
Observer location: undefined°, undefined°
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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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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Authenticating...
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