ELECTRON R/B, 62933 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 62933 was space debris in LEO originally from a launch on Sat, 08 Feb 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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62933 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, Unknown HBR
Radar Cross Section
2.827 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 months ago
TLE from 7 months ago
0 ELECTRON R/B
1 62933U 25028F 25051.88207345 .13714693 21991-5 27058-3 0 9996
2 62933 97.9272 109.5562 0054540 197.5517 275.2945 16.39810484 1876Epoch: 2025-02-20T21:10Z
TLE epoch observation values (Epoch: 2025-02-20T21:10:11.146Z)
Latitude
66.56626°
Longitude
-160.41429°
Altitude
174.739 km
Speed
7.81 km/s
True Right ascension
20h 32m 44s
True Declination
66° 25' 45"
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
04:51:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
198.815 km
Perigee altitude
127.463 km
Semi-major axis
6,541.276 km
Eccentricity
0.00545
Inclination
97.9272°
RAAN
109.5562°
Arg. of periapsis
197.5517°
True anomaly
274.6718°
Mean anomaly
275.2945°
Eccentric anomaly
274.98319°
Mean motion
4.10251 °/min
Orbital period
87.75 mins
BSTAR
0.00027058
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Other satellites on launch #28 in the year 2025 (2025-02-08 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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