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 (1 year ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 5.4 m
Radar Cross Section
39.980 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 FALCON 9 R/B
1 62484U 25001B   26146.35224642 -.00000187  00000-0  13170-2 0  9990
2 62484  25.0512 215.0527 7903793 354.9044   0.6051  1.41763798  7195
Epoch: 2026-05-26T08:27Z
TLE epoch observation values (Epoch: 2026-05-26T08:27:14.090Z)
Latitude
-0.00009°
Longitude
-155.67122°
Altitude
625.225 km
Speed
10.095 km/s
True Right ascension
14h 20m 15s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
11:47:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
53,558.34 km
Perigee altitude
639.329 km
Semi-major axis
33,476.972 km
Eccentricity
0.79038
Inclination
25.0512°
RAAN
215.0527°
Arg. of periapsis
354.9044°
True anomaly
8.40949°
Mean anomaly
0.6051°
Eccentric anomaly
2.88206°
Mean motion
0.35434 °/min
Orbital period
1,015.96 mins
BSTAR
0.001317
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Other satellites on launch #1 in the year 2025 (2025-01-04 UTC)

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