ELECTRON R/B, 64693 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 64693 was space debris in LEO originally from a launch on Sat, 28 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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64693 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, 1.1 m
Radar Cross Section
2.827 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 ELECTRON R/B
1 64693U 25140C 25194.36318463 .26975377 11714-5 35632-3 0 9992
2 64693 95.9461 40.8237 0033637 175.9440 313.4032 16.46008519 2378Epoch: 2025-07-13T08:42Z
TLE epoch observation values (Epoch: 2025-07-13T08:42:59.152Z)
Latitude
50.66513°
Longitude
165.84895°
Altitude
143.089 km
Speed
7.834 km/s
True Right ascension
15h 12m 19s
True Declination
50° 28' 50"
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
10:17:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
168.555 km
Perigee altitude
124.661 km
Semi-major axis
6,524.745 km
Eccentricity
0.00336
Inclination
95.9461°
RAAN
40.8237°
Arg. of periapsis
175.944°
True anomaly
313.12235°
Mean anomaly
313.4032°
Eccentric anomaly
313.26285°
Mean motion
4.11811 °/min
Orbital period
87.42 mins
BSTAR
0.00035632
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Other satellites on launch #140 in the year 2025 (2025-06-28 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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