ELECTRON R/B, 64626 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 64626 was space debris in SSO originally from a launch on Thu, 26 Jun 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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64626 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 64626U 25138F 25181.60997256 .03297959 24869-5 12609-2 0 9992
2 64626 97.4237 186.5515 0179629 21.1293 339.7765 15.96552279 608Epoch: 2025-06-30T14:38Z
TLE epoch observation values (Epoch: 2025-06-30T14:38:21.629Z)
Latitude
0.04997°
Longitude
48.03759°
Altitude
175.123 km
Speed
7.866 km/s
True Right ascension
12h 26m 10s
True Declination
0° 02' 59"
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
07:20:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
400.471 km
Perigee altitude
161.242 km
Semi-major axis
6,658.993 km
Eccentricity
0.01796
Inclination
97.4237°
RAAN
186.5515°
Arg. of periapsis
21.1293°
True anomaly
339.04967°
Mean anomaly
339.7765°
Eccentric anomaly
339.41463°
Mean motion
3.9942 °/min
Orbital period
90.13 mins
BSTAR
0.0012609
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Other satellites on launch #138 in the year 2025 (2025-06-26 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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