DECAYED

ELECTRON R/B, 60354 (Decayed)

Orbit data source: Space-Track

ELECTRON R/B, 60354 was space debris in LEO originally from a launch on Fri, 02 Aug 2024 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
60354, 2024-137C
Orbit
Decayed
Last TLE update
9 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)
2024-08-02 (9 months ago)
Launch vehicle
Unknown
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history

TLE from 9 months ago
0 ELECTRON R/B
1 60354U 24137C   24227.06252620  .07493103  93388-5  13989-2 0  9990
2 60354  42.9539  69.9603 0070986 335.3226 163.4768 16.23819940  1794
Epoch: 2024-08-14T01:30Z
Definitive object data (Epoch: 2024-08-14T01:30:02.263Z)
Latitude
26.63756°
Longitude
-127.91036°
Altitude
254.083 km
Speed
7.733 km/s
True Right ascension
14h 30m 16s
True Declination
26° 29' 22"
Sunlit
Object was in daylight at TLE epoch
Visualization observer readout
Visualization observer readout
Orbital elements
Apogee altitude
258.01 km
Perigee altitude
164.459 km
Semi-major axis
6,589.372 km
Eccentricity
0.0070986
Inclination
42.9539°
RAAN
69.9603°
Arg. of periapsis
335.3226°
True anomaly
163.70619°
Mean anomaly
163.4768°
Eccentric anomaly
163.59169°
Mean motion
4.05767 °/min
BSTAR
0.0013989
Orbital period
88.72 mins
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Other satellites on launch #137 in the year 2024 (2024-08-02 UTC)

ELECTRON R/B Visibility forecast

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