DECAYED

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.

Not visible in the next 10 days
Identifier
63206, 2025-050B
Orbit
Decayed
Last TLE update
1 month ago
Origin
Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
ELECTRON ST2, Unknown motor
Mass
250 kg wet, ~250 kg dry
Launch date (UTC)
2025-03-15 (2 months ago)
Launch vehicle
Unknown
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, Unknown HBR
Radar Cross Section
2.827 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 month 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  3940
Epoch: 2025-04-09T00:26Z
Definitive object data (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
Object was in daylight at TLE epoch
Visualization observer readout
Visualization observer readout
Orbital elements
Apogee altitude
247.941 km
Perigee altitude
179.159 km
Semi-major axis
6,591.687 km
Eccentricity
0.0052173
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
BSTAR
0.0018281
Orbital period
88.77 mins
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Other satellites on launch #50 in the year 2025 (2025-03-15 UTC)

ELECTRON R/B Visibility forecast

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