FALCON 9 R/B, 62260

Orbit data source: Space-Track

FALCON 9 R/B, 62260 is space debris in HEO originally from a launch on Thu, 05 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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Identifier
62260, 2024-234B
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
SpaceX
Mission
Spacecraft
Bus & Motor
F9ST2, Unknown motor
Mass
~4,000 kg wet, ~4,000 kg dry
Launch date (UTC)
2024-12-05 (1 year ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 7.8 m
Radar Cross Section
39.980 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 FALCON 9 R/B
1 62260U 24234B   25352.35767336  .00034560 -49315-6  87917-3 0  9990
2 62260  27.1069 235.0131 5958919 276.1387  23.0986  4.18657792 14707
Epoch: 2025-12-18T08:35Z
TLE epoch observation values (Epoch: 2025-12-18T08:35:02.978Z)
Latitude
0.00029°
Longitude
19.08784°
Altitude
3,499.89 km
Speed
7.496 km/s
True Right ascension
15h 40m 15s
True Declination
0° 00' 01"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
15:32:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,579.329 km
Perigee altitude
194.753 km
Semi-major axis
16,265.178 km
Eccentricity
0.59589
Inclination
27.1069°
RAAN
235.0131°
Arg. of periapsis
276.1387°
True anomaly
84.03968°
Mean anomaly
23.0986°
Eccentric anomaly
48.77962°
Mean motion
1.0463 °/min
Orbital period
344.07 mins
BSTAR
0.00087917
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Other satellites on launch #234 in the year 2024 (2024-12-05 UTC)

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