ELECTRON R/B, 59882 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 59882 was space debris in LEO originally from a launch on Sat, 25 May 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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59882 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
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 ELECTRON R/B
1 59882U 24099B 24162.35253499 .26591496 21862-5 37978-3 0 9994
2 59882 97.4512 21.7750 0027981 183.1273 235.1261 16.46282928 2545Epoch: 2024-06-10T08:27Z
TLE epoch observation values (Epoch: 2024-06-10T08:27:39.023Z)
Latitude
57.33377°
Longitude
-16.02835°
Altitude
169.334 km
Speed
7.804 km/s
True Right ascension
00h 40m 17s
True Declination
57° 09' 48"
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
23:04:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
164.199 km
Perigee altitude
127.689 km
Semi-major axis
6,524.081 km
Eccentricity
0.0028
Inclination
97.4512°
RAAN
21.775°
Arg. of periapsis
183.1273°
True anomaly
234.86357°
Mean anomaly
235.1261°
Eccentric anomaly
234.99478°
Mean motion
4.11874 °/min
Orbital period
87.41 mins
BSTAR
0.00037978
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Other satellites on launch #99 in the year 2024 (2024-05-25 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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