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: 2 days ago

TLE from 2 days ago
0 FALCON 9 R/B
1 62484U 25001B   25359.69524719 -.00000040  00000-0 -12844-2 0  9996
2 62484  25.1997 244.9191 7903149 303.8138   4.9001  1.41762687  5043
Epoch: 2025-12-25T16:41Z
TLE epoch observation values (Epoch: 2025-12-25T16:41:09.357Z)
Latitude
0.00125°
Longitude
-99.61799°
Altitude
2,414.037 km
Speed
8.875 km/s
True Right ascension
16h 20m 28s
True Declination
0° 00' 04"
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
01:55:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
53,556.463 km
Perigee altitude
641.518 km
Semi-major axis
33,477.128 km
Eccentricity
0.79031
Inclination
25.1997°
RAAN
244.9191°
Arg. of periapsis
303.8138°
True anomaly
58.00366°
Mean anomaly
4.9001°
Eccentric anomaly
21.48451°
Mean motion
0.35434 °/min
Orbital period
1,015.97 mins
BSTAR
-0.0012844
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Other satellites on launch #1 in the year 2025 (2025-01-04 UTC)

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