DECAYED

ELECTRON R/B, 62087 (Decayed)

Orbit data source: Space-Track

ELECTRON R/B, 62087 was space debris in LEO originally from a launch on Mon, 25 Nov 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
62087, 2024-219G
Orbit
Decayed
Last TLE update
5 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)
2024-11-25 (6 months ago)
Launch vehicle
Unknown
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Trunc Cone, 1.4 m
Radar Cross Section
0.760 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 5 months ago
0 ELECTRON R/B
1 62087U 24219G   24342.74472910  .24207401  22635-5  35868-3 0  9996
2 62087  97.9193 143.6896 0043756 196.3431 294.5419 16.43612336  1989
Epoch: 2024-12-07T17:52Z
Definitive object data (Epoch: 2024-12-07T17:52:24.594Z)
Latitude
49.04446°
Longitude
-12.23624°
Altitude
152.287 km
Speed
7.827 km/s
True Right ascension
22h 11m 26s
True Declination
48° 51' 30"
Sunlit
Object was in daylight at TLE epoch
Visualization observer readout
Visualization observer readout
Orbital elements
Apogee altitude
181.616 km
Perigee altitude
124.46 km
Semi-major axis
6,531.175 km
Eccentricity
0.0043756
Inclination
97.9193°
RAAN
143.6896°
Arg. of periapsis
196.3431°
True anomaly
294.08476°
Mean anomaly
294.5419°
Eccentric anomaly
294.31343°
Mean motion
4.11203 °/min
BSTAR
0.00035868
Orbital period
87.55 mins
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ELECTRON R/B Visibility forecast

Observer location: undefined°, undefined°

This satellite is decayed
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