FALCON 9 R/B, 62484

Orbit data source: Space-Track

FALCON 9 R/B, 62484 is space debris in HEO originally from a launch on Sat, 04 Jan 2025 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
62484, 2025-001B
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)
2025-01-04 (2 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 8.0 m
Radar Cross Section
39.980 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago
0 FALCON 9 R/B
1 62484U 25001B   26306.46442784  .00000489  00000-0  24643-2 0  9990
2 62484  24.1150 181.3735 7984818  51.7889 356.0576  1.41798781  9467
Epoch: 2026-11-02T11:08Z
TLE epoch observation values (Epoch: 2026-11-02T11:08:46.565Z)
Latitude
-0.0005°
Longitude
-27.35047°
Altitude
1,685.326 km
Speed
9.325 km/s
True Right ascension
12h 06m 20s
True Declination
0° 00' 02"
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
00:23:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
53,820.292 km
Perigee altitude
367.041 km
Semi-major axis
33,471.804 km
Eccentricity
0.79848
Inclination
24.115°
RAAN
181.3735°
Arg. of periapsis
51.7889°
True anomaly
308.53154°
Mean anomaly
356.0576°
Eccentric anomaly
341.66925°
Mean motion
0.35443 °/min
Orbital period
1,015.73 mins
BSTAR
0.0024643
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Other satellites on launch #1 in the year 2025 (2025-01-04 UTC)

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