FALCON 9 R/B, 62260
Orbit data source: Space-Track
FALCON 9 R/B, 62260 is space debris in HEO originally from a launch on Thu, 05 Dec 2024 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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62260 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 FALCON 9 R/B
1 62260U 24234B 25239.36024792 .00057692 82618-7 13605-2 0 9993
2 62260 27.1910 324.7426 6033594 127.1779 304.5376 4.07514745 10028
Epoch: 2025-08-27T08:38Z
TLE epoch observation values (Epoch: 2025-08-27T08:38:45.42Z)
Latitude
0.00012°
Longitude
-140.76992°
Altitude
10,195.932 km
Speed
4.902 km/s
True Right ascension
21h 39m 01s
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
16:26:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
20,173.946 km
Perigee altitude
190.343 km
Semi-major axis
16,560.282 km
Eccentricity
0.60336
Inclination
27.191°
RAAN
324.7426°
Arg. of periapsis
127.1779°
True anomaly
232.86334°
Mean anomaly
304.5376°
Eccentric anomaly
269.96766°
Mean motion
1.01845 °/min
Orbital period
353.48 mins
BSTAR
0.0013605
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Other satellites on launch #234 in the year 2024 (2024-12-05 UTC)
FALCON 9 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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87 mins | 2025-08-28 07:26:42.362Z | 226.541° WSW | 2025-08-28 08:43:42.362Z | 177.87° S | 31.915° | 2025-08-28 08:53:42.362Z | 113.661° SE |
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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