FALCON 9 R/B, 56175

Orbit data source: Space-Track

FALCON 9 R/B, 56175 is space debris in HEO originally from a launch on Fri, 07 Apr 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
56175, 2023-052B
Orbit
HEO
Last TLE update
2 days ago
Origin
Manufacturer
SpaceX
Mission
Spacecraft
Bus & Motor
F9ST2, Unknown motor
Mass
~3,000 kg wet, ~3,000 kg dry
Launch date (UTC)
2023-04-07 (2 years 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

TLE from 2 days ago
0 FALCON 9 R/B
1 56175U 23052B   25198.06234289  .00024919  00000-0  10241-2 0  9990
2 56175  27.1418 356.6335 6350715 221.7574  66.7433  3.58696547 25879
Epoch: 2025-07-17T01:29Z
TLE epoch observation values (Epoch: 2025-07-17T01:29:46.425Z)
Latitude
-0.00007°
Longitude
39.05059°
Altitude
14,066.932 km
Speed
4.109 km/s
True Right ascension
23h 46m 30s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
27.15355°
Longitude
124.79215°
Altitude
13,617.919 km
Speed
4.214 km/s
Apparent Right ascension
05h 28m 11s
Apparent Declination
12° 30' 55"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
17:23:31
Azimuth
358.564° N
Elevation
-37.557°
Doppler factor
1
Orbital elements
Apogee altitude
23,102.842 km
Perigee altitude
201.667 km
Semi-major axis
18,030.391 km
Eccentricity
0.63507
Inclination
27.1418°
RAAN
356.6335°
Arg. of periapsis
221.7574°
True anomaly
138.33124°
Mean anomaly
66.7433°
Eccentric anomaly
102.29557°
Mean motion
0.89647 °/min
Orbital period
401.58 mins
BSTAR
0.0010241
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