FALCON HEAVY R/B, 56373

Orbit data source: Space-Track

FALCON HEAVY R/B, 56373 is space debris in GEO originally from a launch on Mon, 01 May 2023 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
56373, 2023-060D
Orbit
GEO
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)
2023-05-01 (2 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, Unknown HBR
Radar Cross Section
49.816 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 FALCON HEAVY R/B
1 56373U 23060D   25247.21565000 -.00000132  00000-0  00000-0 0  9991
2 56373   2.1352  81.8525 0014225 165.0968  65.7130  1.04744407  8974
Epoch: 2025-09-04T05:10Z
TLE epoch observation values (Epoch: 2025-09-04T05:10:32.16Z)
Latitude
-1.65799°
Longitude
-108.43253°
Altitude
34,553.491 km
Speed
3.122 km/s
True Right ascension
20h 51m 07s
True Declination
-1° 39' 23"
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
08:39:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,636.947 km
Perigee altitude
34,520.425 km
Semi-major axis
40,956.823 km
Eccentricity
0.00142
Inclination
2.1352°
RAAN
81.8525°
Arg. of periapsis
165.0968°
True anomaly
65.86169°
Mean anomaly
65.713°
Eccentric anomaly
65.78733°
Mean motion
0.26185 °/min
Orbital period
1,374.83 mins
BSTAR
0
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Other satellites on launch #60 in the year 2023 (2023-05-01 UTC)

Documentation

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