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 (10 months 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: 14 hours ago

TLE from 14 hours ago
0 FALCON 9 R/B
1 62260U 24234B   25291.63183266  .00056396 -17004-6  13512-2 0  9997
2 62260  27.1512 283.7024 5995413 195.3652 132.6127  4.13276862 12171
Epoch: 2025-10-18T15:09Z
TLE epoch observation values (Epoch: 2025-10-18T15:09:50.341Z)
Latitude
-0°
Longitude
28.86565°
Altitude
18,515.805 km
Speed
2.779 km/s
True Right ascension
18h 54m 44s
True Declination
0° 00' 00"
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
00:15:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,863.98 km
Perigee altitude
191.799 km
Semi-major axis
16,406.027 km
Eccentricity
0.59954
Inclination
27.1512°
RAAN
283.7024°
Arg. of periapsis
195.3652°
True anomaly
164.65426°
Mean anomaly
132.6127°
Eccentric anomaly
149.86061°
Mean motion
1.03285 °/min
Orbital period
348.55 mins
BSTAR
0.0013512
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Other satellites on launch #234 in the year 2024 (2024-12-05 UTC)

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