FALCON 9 R/B, 58699
Orbit data source: Space-Track
FALCON 9 R/B, 58699 is space debris in HEO originally from a launch on Wed, 03 Jan 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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58699 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 1 day ago
0 FALCON 9 R/B
1 58699U 24003B 25197.99201073 .00000334 00000-0 52960-3 0 9996
2 58699 25.4221 148.5309 7748775 65.0889 353.5089 1.68490883 9421
Epoch: 2025-07-16T23:48Z
TLE epoch observation values (Epoch: 2025-07-16T23:48:29.727Z)
Latitude
0.00016°
Longitude
-143.80189°
Altitude
2,645.468 km
Speed
8.659 km/s
True Right ascension
09h 53m 32s
True Declination
0° 00' 01"
Sunlit
Visualization orbit readout
Latitude
-18.67605°
Longitude
81.18178°
Altitude
39,235.467 km
Speed
2.029 km/s
Apparent Right ascension
01h 15m 55s
Apparent Declination
-24° 43' 34"
Sunlit
Visualization observer readout
Local Sidereal Time
21:17:24
Azimuth
128.144° SE
Elevation
4.807°
Doppler factor
1
Orbital elements
Apogee altitude
46,577.776 km
Perigee altitude
338.703 km
Semi-major axis
29,836.376 km
Eccentricity
0.77488
Inclination
25.4221°
RAAN
148.5309°
Arg. of periapsis
65.0889°
True anomaly
294.41337°
Mean anomaly
353.5089°
Eccentric anomaly
334.15323°
Mean motion
0.42114 °/min
Orbital period
854.83 mins
BSTAR
0.0005296
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Other satellites on launch #3 in the year 2024 (2024-01-03 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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493 mins | 2025-07-18 09:49:14.485Z | 138.349° SSE | 2025-07-18 13:28:14.485Z | 171.698° S | 17.39° | 2025-07-18 18:02:14.485Z | 177.354° S |
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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