FALCON 9 R/B, 62007
Orbit data source: Space-Track
FALCON 9 R/B, 62007 is space debris in HEO originally from a launch on Sun, 17 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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62007 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 FALCON 9 R/B
1 62007U 24212B 26061.49838326 -.00000127 00000-0 85477-3 0 9999
2 62007 18.3213 95.7934 7801966 45.5504 356.3670 1.58893278 7426Epoch: 2026-03-02T11:57Z
TLE epoch observation values (Epoch: 2026-03-02T11:57:40.313Z)
Latitude
-0.00019°
Longitude
116.32453°
Altitude
1,419.429 km
Speed
9.454 km/s
True Right ascension
06h 24m 08s
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
07:12:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
48,855.32 km
Perigee altitude
441.616 km
Semi-major axis
31,026.605 km
Eccentricity
0.7802
Inclination
18.3213°
RAAN
95.7934°
Arg. of periapsis
45.5504°
True anomaly
316.85708°
Mean anomaly
356.367°
Eccentric anomaly
344.18209°
Mean motion
0.39714 °/min
Orbital period
906.49 mins
BSTAR
0.00085477
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Other satellites on launch #212 in the year 2024 (2024-11-17 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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