ELECTRON R/B, 63206 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 63206 was space debris in LEO originally from a launch on Sat, 15 Mar 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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63206 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: 5 months ago
TLE from 5 months ago
0 ELECTRON R/B
1 63206U 25050B 25099.01834074 .06663047 83338-5 18281-2 0 9995
2 63206 42.0012 313.1202 0052173 87.6824 29.0083 16.23025334 3940Epoch: 2025-04-09T00:26Z
TLE epoch observation values (Epoch: 2025-04-09T00:26:24.639Z)
Latitude
36.75326°
Longitude
-126.54416°
Altitude
182.958 km
Speed
7.82 km/s
True Right ascension
05h 10m 16s
True Declination
36° 34' 27"
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
23:44:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
247.941 km
Perigee altitude
179.159 km
Semi-major axis
6,591.687 km
Eccentricity
0.00522
Inclination
42.0012°
RAAN
313.1202°
Arg. of periapsis
87.6824°
True anomaly
29.29988°
Mean anomaly
29.0083°
Eccentric anomaly
29.15393°
Mean motion
4.05554 °/min
Orbital period
88.77 mins
BSTAR
0.0018281
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Other satellites on launch #50 in the year 2025 (2025-03-15 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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