FALCON 9 R/B, 52818
Orbit data source: Space-Track
FALCON 9 R/B, 52818 is space debris in HEO originally from a launch on Wed, 08 Jun 2022 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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52818 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 FALCON 9 R/B
1 52818U 22061B 25354.78800287 .00000180 00000-0 51973-3 0 9991
2 52818 18.6249 24.3285 7626034 157.8678 272.0467 1.81900989 23075Epoch: 2025-12-20T18:54Z
TLE epoch observation values (Epoch: 2025-12-20T18:54:43.447Z)
Latitude
0.00005°
Longitude
11.01792°
Altitude
34,060.626 km
Speed
2.377 km/s
True Right ascension
01h 37m 14s
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
13:58:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
43,595.523 km
Perigee altitude
352.576 km
Semi-major axis
28,352.186 km
Eccentricity
0.7626
Inclination
18.6249°
RAAN
24.3285°
Arg. of periapsis
157.8678°
True anomaly
202.02699°
Mean anomaly
272.0467°
Eccentric anomaly
235.87581°
Mean motion
0.45464 °/min
Orbital period
791.84 mins
BSTAR
0.00051973
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Other satellites on launch #61 in the year 2022 (2022-06-08 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
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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