DECAYED

ELECTRON R/B, 59966 (Decayed)

Orbit data source: Space-Track

ELECTRON R/B, 59966 was space debris in LEO originally from a launch on Wed, 05 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
59966, 2024-108B
Orbit
Decayed
Last TLE update
11 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)
2024-06-05 (11 months ago)
Launch vehicle
Unknown
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history

TLE from 11 months ago
0 ELECTRON R/B
1 59966U 24108B   24170.49493666  .30482529  21787-5  32658-3 0  9991
2 59966  97.4760 323.0336 0030815 193.7375 210.7109 16.47875042  2110
Epoch: 2024-06-18T11:52Z
Definitive object data (Epoch: 2024-06-18T11:52:42.527Z)
Latitude
43.89776°
Longitude
-129.57075°
Altitude
168.957 km
Speed
7.799 km/s
True Right ascension
21h 03m 17s
True Declination
43° 42' 38"
Sunlit
Object was in daylight at TLE epoch
Visualization observer readout
Visualization observer readout
Orbital elements
Apogee altitude
161.829 km
Perigee altitude
121.647 km
Semi-major axis
6,519.875 km
Eccentricity
0.0030815
Inclination
97.476°
RAAN
323.0336°
Arg. of periapsis
193.7375°
True anomaly
210.53116°
Mean anomaly
210.7109°
Eccentric anomaly
210.62097°
Mean motion
4.12272 °/min
BSTAR
0.00032658
Orbital period
87.32 mins
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Other satellites on launch #108 in the year 2024 (2024-06-05 UTC)

ELECTRON R/B Visibility forecast

Observer location: undefined°, undefined°

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