FALCON 9 R/B, 43563
Orbit data source: Space-Track
FALCON 9 R/B, 43563 is space debris originally from a launch on Sun, 22 Jul 2018 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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43563 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 FALCON 9 R/B
1 43563U 18059B 25295.94907179 .00077083 00000-0 15004-2 0 9990
2 43563 26.9460 123.4854 4300220 92.6498 315.7621 6.97996016140469
Epoch: 2025-10-22T22:46Z
TLE epoch observation values (Epoch: 2025-10-22T22:46:39.802Z)
Latitude
0.00002°
Longitude
110.20424°
Altitude
3,235.048 km
Speed
6.962 km/s
True Right ascension
08h 13m 56s
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
03:56:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
10,165.996 km
Perigee altitude
216.021 km
Semi-major axis
11,569.146 km
Eccentricity
0.43002
Inclination
26.946°
RAAN
123.4854°
Arg. of periapsis
92.6498°
True anomaly
267.40057°
Mean anomaly
315.7621°
Eccentric anomaly
293.09895°
Mean motion
1.74418 °/min
Orbital period
206.4 mins
BSTAR
0.0015004
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Other satellites on launch #59 in the year 2018 (2018-07-22 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 9 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 9 R/B is likely not visible in the next few days. |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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