FALCON 9 R/B, 61732
Orbit data source: Space-Track
FALCON 9 R/B, 61732 is space debris in LEO originally from a launch on Mon, 07 Oct 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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61732 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 FALCON 9 R/B
1 61732U 24180B 24281.62491802 -.00000101 32184-6 00000-0 0 9990
2 61732 34.1400 34.7539 0027900 134.8400 359.2800 16.36805402 04
Epoch: 2024-10-07T14:59Z
TLE epoch observation values (Epoch: 2024-10-07T14:59:52.916Z)
Latitude
23.8652°
Longitude
-67.40956°
Altitude
154.724 km
Speed
7.829 km/s
True Right ascension
11h 37m 14s
True Declination
23° 43' 35"
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
00:51:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
196.157 km
Perigee altitude
159.575 km
Semi-major axis
6,556.003 km
Eccentricity
0.00279
Inclination
34.14°
RAAN
34.7539°
Arg. of periapsis
134.84°
True anomaly
359.27597°
Mean anomaly
359.28°
Eccentric anomaly
359.27799°
Mean motion
4.08869 °/min
Orbital period
88.05 mins
BSTAR
0
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Other satellites on launch #180 in the year 2024 (2024-10-07 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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