FALCON 9 R/B, 62458 (Decayed)
Orbit data source: Space-Track
FALCON 9 R/B, 62458 was space debris in LEO originally from a launch on Sun, 29 Dec 2024 UTC launched from the Air Force Eastern Test Range (AFETR). 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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62458 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX
Mission
Decayed spacecraft
Bus & Motor
F9ST2, Unknown motor
Mass
~3,000 kg wet, ~3,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 7.8 m
Radar Cross Section
39.980 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 months ago
TLE from 3 months ago
0 FALCON 9 R/B
1 62458U 24252E 25145.84930473 .67595417 -50746-4 25604-2 0 9995
2 62458 12.2742 275.6558 1715914 343.7064 190.6692 12.53828150 3290Epoch: 2025-05-25T20:22Z
TLE epoch observation values (Epoch: 2025-05-25T20:22:59.928Z)
Latitude
1.83016°
Longitude
-102.17445°
Altitude
2,771.198 km
Speed
6.02 km/s
True Right ascension
05h 48m 58s
True Declination
1° 49' 18"
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
05:50:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,797.948 km
Perigee altitude
110.087 km
Semi-major axis
7,832.154 km
Eccentricity
0.17159
Inclination
12.2742°
RAAN
275.6558°
Arg. of periapsis
343.7064°
True anomaly
187.66701°
Mean anomaly
190.6692°
Eccentric anomaly
189.11221°
Mean motion
3.13128 °/min
Orbital period
114.97 mins
BSTAR
0.0025604
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Other satellites on launch #252 in the year 2024 (2024-12-29 UTC)
FALCON 9 R/B Visibility
Observer location: undefined°, undefined°
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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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Authenticating...
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