DECAYED

ELECTRON R/B, 60080 (Decayed)

Orbit data source: Space-Track

ELECTRON R/B, 60080 was space debris in LEO originally from a launch on Thu, 20 Jun 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
60080, 2024-114B
Orbit
Decayed
Last TLE update
1 year ago
Origin
Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
ELECTRON ST2, Unknown motor
Mass
250 kg wet, ~250 kg dry
Launch date (UTC)
2024-06-20 (1 year 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 year ago
0 ELECTRON R/B
1 60080U 24114B   24191.33362157  .03351378  28213-5  10000-3 0  9998
2 60080  97.9887 210.0944 0037508 162.4915 323.4653 16.40261238  2916
Epoch: 2024-07-09T08:00Z
TLE epoch observation values (Epoch: 2024-07-09T08:00:24.903Z)
Latitude
53.64462°
Longitude
-6.83655°
Altitude
154.298 km
Speed
7.831 km/s
True Right ascension
02h 44m 05s
True Declination
53° 27' 54"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Visualization observer readout
Orbital elements
Apogee altitude
186.473 km
Perigee altitude
137.412 km
Semi-major axis
6,540.079 km
Eccentricity
0.00375
Inclination
97.9887°
RAAN
210.0944°
Arg. of periapsis
162.4915°
True anomaly
Unknown
Mean anomaly
323.4653°
Eccentric anomaly
Unknown
Mean motion
4.10363 °/min
Orbital period
87.73 mins
BSTAR
0.0001
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ELECTRON R/B Visibility

Observer location: undefined°, undefined°

This satellite is decayed
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