DECAYED

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.

Not visible in the next 10 days
Identifier
62933, 2025-028F
Orbit
Decayed
Last TLE update
3 months ago
Origin
Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
ELECTRON ST2, Unknown motor
Mass
250 kg wet, ~250 kg dry
Launch date (UTC)
2025-02-08 (3 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 3 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  1876
Epoch: 2025-02-20T21:10Z
Definitive object data (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
Object was in daylight at TLE epoch
Visualization observer readout
Visualization observer readout
Orbital elements
Apogee altitude
198.815 km
Perigee altitude
127.463 km
Semi-major axis
6,541.276 km
Eccentricity
0.005454
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
BSTAR
0.00027058
Orbital period
87.75 mins
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ELECTRON R/B Visibility forecast

Observer location: undefined°, undefined°

This satellite is decayed
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