FALCON HEAVY DEB, 55266
Orbit data source: Space-Track
FALCON HEAVY DEB, 55266 is space debris in GEO originally from a launch on Sun, 15 Jan 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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55266 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 FALCON HEAVY DEB
1 55266U 23008D 25346.02349414 .00000024 00000-0 00000-0 0 9990
2 55266 2.6786 80.3649 0009971 80.4304 279.2983 1.02406286 6117Epoch: 2025-12-12T00:33Z
TLE epoch observation values (Epoch: 2025-12-12T00:33:49.893Z)
Latitude
-0°
Longitude
-9.45051°
Altitude
35,191.448 km
Speed
3.097 km/s
True Right ascension
05h 19m 54s
True Declination
0° 00' 00"
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
07:35:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,241.173 km
Perigee altitude
35,158.259 km
Semi-major axis
41,577.853 km
Eccentricity
0.001
Inclination
2.6786°
RAAN
80.3649°
Arg. of periapsis
80.4304°
True anomaly
279.18552°
Mean anomaly
279.2983°
Eccentric anomaly
279.24191°
Mean motion
0.25601 °/min
Orbital period
1,406.22 mins
BSTAR
0
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Other satellites on launch #8 in the year 2023 (2023-01-15 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.FALCON HEAVY DEB Visibility
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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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| FALCON HEAVY DEB is likely not visible in the next few days. |
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55266 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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