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: 1 day ago

TLE from 1 day ago
0 FALCON 9 R/B
1 62484U 25001B   26056.06202900 -.00000150  00000-0  94773-3 0  9990
2 62484  25.2764 232.8417 7894256 324.4011   2.4358  1.41762218  5914
Epoch: 2026-02-25T01:29Z
TLE epoch observation values (Epoch: 2026-02-25T01:29:19.305Z)
Latitude
-0.00003°
Longitude
55.62059°
Altitude
1,317.98 km
Speed
9.574 km/s
True Right ascension
15h 31m 32s
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
06:20:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
53,526.767 km
Perigee altitude
671.298 km
Semi-major axis
33,477.169 km
Eccentricity
0.78943
Inclination
25.2764°
RAAN
232.8417°
Arg. of periapsis
324.4011°
True anomaly
32.15787°
Mean anomaly
2.4358°
Eccentric anomaly
11.29377°
Mean motion
0.35434 °/min
Orbital period
1,015.97 mins
BSTAR
0.00094773
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Other satellites on launch #1 in the year 2025 (2025-01-04 UTC)

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