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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56373 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast 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
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
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)
FALCON HEAVY R/B Visibility forecast
Observer location: undefined°, undefined°
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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1440 mins | 2025-09-04 16:43:56.763Z | 173.326° S | 2025-09-04 18:45:56.763Z | 171.051° S | 35.57° | 2025-09-05 16:43:56.763Z | 148.967° SSE |
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56373 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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