FALCON HEAVY R/B, 55265
Orbit data source: Space-Track
FALCON HEAVY R/B, 55265 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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55265 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 FALCON HEAVY R/B
1 55265U 23008C 26105.41209491 -.00000164 00000-0 00000-0 0 9992
2 55265 2.7216 76.2226 0053581 74.8508 286.0200 1.03135554 7240Epoch: 2026-04-15T09:53Z
TLE epoch observation values (Epoch: 2026-04-15T09:53:25.000Z)
Latitude
-0°
Longitude
84.56494°
Altitude
34,942.98 km
Speed
3.108 km/s
True Right ascension
05h 05m 58s
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
04:39:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,225.224 km
Perigee altitude
34,781.77 km
Semi-major axis
41,381.634 km
Eccentricity
0.00536
Inclination
2.7216°
RAAN
76.2226°
Arg. of periapsis
74.8508°
True anomaly
285.42877°
Mean anomaly
286.02°
Eccentric anomaly
285.72449°
Mean motion
0.25783 °/min
Orbital period
1,396.27 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 R/B 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 R/B is likely not visible in the next few days. |
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55265 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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