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.
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60080 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
Cyl, Unknown HBR
Radar Cross Section
2.827 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
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 2916Epoch: 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
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
10:54:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
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
323.20846°
Mean anomaly
323.4653°
Eccentric anomaly
323.33698°
Mean motion
4.10363 °/min
Orbital period
87.73 mins
BSTAR
0.0001
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Other satellites on launch #114 in the year 2024 (2024-06-20 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ELECTRON R/B Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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