ELECTRON R/B, 63360 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 63360 was space debris in LEO originally from an American launch on Wed, 26 Mar 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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63360 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
None
Manufacturer
Unknown
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Trunc Cone, 0.7 m
Radar Cross Section
0.760 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 months ago
TLE from 6 months ago
0 ELECTRON R/B
1 63360U 25061K 25093.91998919 .15544858 16667-5 57746-3 0 9999
2 63360 97.4778 71.5023 0070408 204.7066 215.7806 16.32848516 1312Epoch: 2025-04-03T22:04Z
TLE epoch observation values (Epoch: 2025-04-03T22:04:47.066Z)
Latitude
59.2903°
Longitude
-104.87232°
Altitude
232.626 km
Speed
7.751 km/s
True Right ascension
03h 55m 14s
True Declination
59° 07' 37"
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
04:01:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
227.903 km
Perigee altitude
135.529 km
Semi-major axis
6,559.853 km
Eccentricity
0.00704
Inclination
97.4778°
RAAN
71.5023°
Arg. of periapsis
204.7066°
True anomaly
215.31222°
Mean anomaly
215.7806°
Eccentric anomaly
215.54608°
Mean motion
4.08509 °/min
Orbital period
88.13 mins
BSTAR
0.00057746
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Other satellites on launch #61 in the year 2025 (2025-03-26 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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