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: 14 hours ago

TLE from 14 hours ago
0 FALCON 9 R/B
1 62260U 24234B   26129.66181731  .00096449  31595-7  17030-2 0  9999
2 62260  27.0934 117.4544 5861946 111.4942 318.5874  4.34803336 20754
Epoch: 2026-05-09T15:53Z
TLE epoch observation values (Epoch: 2026-05-09T15:53:01.015Z)
Latitude
0.00001°
Longitude
11.71952°
Altitude
6,863.255 km
Speed
5.922 km/s
True Right ascension
07h 49m 47s
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
13:35:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,779.039 km
Perigee altitude
184.85 km
Semi-major axis
15,860.081 km
Eccentricity
0.58619
Inclination
27.0934°
RAAN
117.4544°
Arg. of periapsis
111.4942°
True anomaly
248.60886°
Mean anomaly
318.5874°
Eccentric anomaly
286.36097°
Mean motion
1.08664 °/min
Orbital period
331.3 mins
BSTAR
0.001703
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Other satellites on launch #234 in the year 2024 (2024-12-05 UTC)

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