FALCON 9 R/B, 61911
Orbit data source: Space-Track
FALCON 9 R/B, 61911 is space debris in HEO originally from a launch on Mon, 11 Nov 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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61911 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 9 R/B
1 61911U 24206B 25341.64020519 .00033282 00000-0 38828-2 0 9993
2 61911 27.6003 358.0651 7197949 67.8136 350.6220 2.40555139 9150Epoch: 2025-12-07T15:21Z
TLE epoch observation values (Epoch: 2025-12-07T15:21:53.728Z)
Latitude
-0.00022°
Longitude
50.94076°
Altitude
2,501.761 km
Speed
8.534 km/s
True Right ascension
23h 52m 15s
True Declination
0° 00' 01"
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
22:12:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,092.407 km
Perigee altitude
215.703 km
Semi-major axis
23,532.192 km
Eccentricity
0.71979
Inclination
27.6003°
RAAN
358.0651°
Arg. of periapsis
67.8136°
True anomaly
292.85253°
Mean anomaly
350.622°
Eccentric anomaly
330.0037°
Mean motion
0.60124 °/min
Orbital period
598.76 mins
BSTAR
0.0038828
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Other satellites on launch #206 in the year 2024 (2024-11-11 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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