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 (10 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: 1 day ago

TLE from 1 day ago
0 FALCON 9 R/B
1 62484U 25001B   25316.66837696 -.00000259  00000-0 -94342-4 0  9994
2 62484  25.1599 253.7668 7920035 288.9841   6.6939  1.41763138  4438
Epoch: 2025-11-12T16:02Z
TLE epoch observation values (Epoch: 2025-11-12T16:02:27.769Z)
Latitude
-0.00072°
Longitude
-39.08242°
Altitude
3,515.544 km
Speed
8.286 km/s
True Right ascension
16h 54m 16s
True Declination
0° 00' 03"
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
16:12:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
53,612.954 km
Perigee altitude
584.984 km
Semi-major axis
33,477.106 km
Eccentricity
0.792
Inclination
25.1599°
RAAN
253.7668°
Arg. of periapsis
288.9841°
True anomaly
72.38097°
Mean anomaly
6.6939°
Eccentric anomaly
27.99267°
Mean motion
0.35434 °/min
Orbital period
1,015.97 mins
BSTAR
-0.000094342
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Other satellites on launch #1 in the year 2025 (2025-01-04 UTC)

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