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 (8 months ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 7.8 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   25256.71427709 -.00000161  00000-0  16691-2 0  9993
2 62484  25.2123 266.7564 7945598 267.4299  10.1678  1.41755637  3581
Epoch: 2025-09-13T17:08Z
TLE epoch observation values (Epoch: 2025-09-13T17:08:33.54Z)
Latitude
-0.00131°
Longitude
16.5971°
Altitude
6,360.432 km
Speed
7.118 km/s
True Right ascension
17h 46m 43s
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
01:42:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
53,700.765 km
Perigee altitude
499.662 km
Semi-major axis
33,478.35 km
Eccentricity
0.79456
Inclination
25.2123°
RAAN
266.7564°
Arg. of periapsis
267.4299°
True anomaly
91.84387°
Mean anomaly
10.1678°
Eccentric anomaly
38.52044°
Mean motion
0.35432 °/min
Orbital period
1,016.03 mins
BSTAR
0.0016691
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Other satellites on launch #1 in the year 2025 (2025-01-04 UTC)

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