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 (9 months 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   25287.04376875 -.00000279  00000-0  13561-2 0  9993
2 62484  25.1753 260.0978 7933587 278.4482   8.1061  1.41762550  4010
Epoch: 2025-10-14T01:03Z
TLE epoch observation values (Epoch: 2025-10-14T01:03:01.620Z)
Latitude
-0.00141°
Longitude
-138.74114°
Altitude
4,656.287 km
Speed
7.767 km/s
True Right ascension
17h 19m 24s
True Declination
0° 00' 05"
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
08:40:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
53,658.551 km
Perigee altitude
539.642 km
Semi-major axis
33,477.234 km
Eccentricity
0.79336
Inclination
25.1753°
RAAN
260.0978°
Arg. of periapsis
278.4482°
True anomaly
81.4676°
Mean anomaly
8.1061°
Eccentric anomaly
32.58951°
Mean motion
0.35434 °/min
Orbital period
1,015.98 mins
BSTAR
0.0013561
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Other satellites on launch #1 in the year 2025 (2025-01-04 UTC)

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