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 week ago

TLE from 1 week ago
0 FALCON 9 R/B
1 62484U 25001B   25303.97202511 -.00000267  00000-0 -84168-3 0  9999
2 62484  25.1638 256.4444 7925512 284.5183   7.2631  1.41763244  4254
Epoch: 2025-10-30T23:19Z
TLE epoch observation values (Epoch: 2025-10-30T23:19:42.969Z)
Latitude
0.00002°
Longitude
-133.27342°
Altitude
3,946.084 km
Speed
8.081 km/s
True Right ascension
17h 04m 42s
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
15:24:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
53,631.286 km
Perigee altitude
566.648 km
Semi-major axis
33,477.104 km
Eccentricity
0.79255
Inclination
25.1638°
RAAN
256.4444°
Arg. of periapsis
284.5183°
True anomaly
76.2527°
Mean anomaly
7.2631°
Eccentric anomaly
29.89792°
Mean motion
0.35434 °/min
Orbital period
1,015.97 mins
BSTAR
-0.00084168
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Other satellites on launch #1 in the year 2025 (2025-01-04 UTC)

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