ELECTRON R/B, 64056 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 64056 was space debris in LEO originally from a launch on Sat, 17 May 2025 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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64056 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, 1.2 m
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 64056U 25104B 25177.00228279 .09650386 79440-5 11816-2 0 9990
2 64056 41.9296 49.7578 0033698 189.0706 313.4381 16.33134775 6249Epoch: 2025-06-26T00:03Z
TLE epoch observation values (Epoch: 2025-06-26T00:03:17.233Z)
Latitude
24.25205°
Longitude
-75.3532°
Altitude
168.577 km
Speed
7.818 km/s
True Right ascension
13h 19m 22s
True Declination
24° 06' 43"
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
07:19:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
208.471 km
Perigee altitude
164.229 km
Semi-major axis
6,564.487 km
Eccentricity
0.00337
Inclination
41.9296°
RAAN
49.7578°
Arg. of periapsis
189.0706°
True anomaly
313.1569°
Mean anomaly
313.4381°
Eccentric anomaly
313.29758°
Mean motion
4.08077 °/min
Orbital period
88.22 mins
BSTAR
0.0011816
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Other satellites on launch #104 in the year 2025 (2025-05-17 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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