ELECTRON R/B, 56445 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 56445 was space debris in LEO originally from a launch on Mon, 08 May 2023 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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56445 intel report (Beta)
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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: 8 months ago
TLE from 8 months ago
0 ELECTRON R/B
1 56445U 23062D 25283.52092476 .05699519 18959-5 18913-2 0 9997
2 56445 35.4611 335.7780 0003724 89.8407 270.2774 16.24717554135528Epoch: 2025-10-10T12:30Z
TLE epoch observation values (Epoch: 2025-10-10T12:30:07.899Z)
Latitude
-0.00003°
Longitude
128.87947°
Altitude
205.673 km
Speed
7.786 km/s
True Right ascension
22h 23m 06s
True Declination
0° 00' 00"
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
21:30:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
212.545 km
Perigee altitude
207.638 km
Semi-major axis
6,588.228 km
Eccentricity
0.00037
Inclination
35.4611°
RAAN
335.778°
Arg. of periapsis
89.8407°
True anomaly
270.23473°
Mean anomaly
270.2774°
Eccentric anomaly
270.25606°
Mean motion
4.05873 °/min
Orbital period
88.7 mins
BSTAR
0.0018913
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Other satellites on launch #62 in the year 2023 (2023-05-08 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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