ELECTRON R/B, 56755 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 56755 was space debris in LEO originally from a launch on Fri, 26 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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56755 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: 1 year ago
TLE from 1 year ago
0 ELECTRON R/B
1 56755U 23073D 25134.83402661 .04905803 19132-5 12008-2 0 9991
2 56755 35.4222 355.4901 0013731 295.0929 159.6376 16.27863882110107Epoch: 2025-05-14T20:00Z
TLE epoch observation values (Epoch: 2025-05-14T20:00:59.899Z)
Latitude
35.43527°
Longitude
-81.70131°
Altitude
207.375 km
Speed
7.783 km/s
True Right ascension
06h 05m 26s
True Declination
35° 15' 34"
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
00:29:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
210.649 km
Perigee altitude
192.58 km
Semi-major axis
6,579.751 km
Eccentricity
0.00137
Inclination
35.4222°
RAAN
355.4901°
Arg. of periapsis
295.0929°
True anomaly
159.69226°
Mean anomaly
159.6376°
Eccentric anomaly
159.66494°
Mean motion
4.06658 °/min
Orbital period
88.53 mins
BSTAR
0.0012008
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Other satellites on launch #73 in the year 2023 (2023-05-26 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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