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.
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62087 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
ELECTRON ST2, Unknown motor
Mass
250 kg wet, ~250 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Trunc Cone, 0.7 m
Radar Cross Section
0.760 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 months ago
TLE from 9 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 1989Epoch: 2024-12-07T17:52Z
TLE epoch observation values (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
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
15:47:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
181.616 km
Perigee altitude
124.46 km
Semi-major axis
6,531.175 km
Eccentricity
0.00438
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
Orbital period
87.55 mins
BSTAR
0.00035868
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Other satellites on launch #219 in the year 2024 (2024-11-25 UTC)
ELECTRON R/B Visibility
Observer location: undefined°, undefined°
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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Authenticating...
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