STARLINK-34343 DEB, 69729
Orbit data source: Space-Track
STARLINK-34343 DEB, 69729 is space debris in SSO originally from a launch on Tue, 27 May 2025 UTC launched from the Air Force Western Test Range (AFWTR). 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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69729 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 2 weeks ago
TLE from 2 weeks ago
0 STARLINK-34343 DEB
1 69729U 25112AA 26176.67516303 .07376444 78813-1 37037-1 0 9991
2 69729 97.5913 230.1636 0026366 256.2010 103.6326 15.86559319 59691Epoch: 2026-06-25T16:12Z
TLE epoch observation values (Epoch: 2026-06-25T16:12:14.085Z)
Latitude
-0.00005°
Longitude
73.2903°
Altitude
319.314 km
Speed
7.714 km/s
True Right ascension
15h 20m 39s
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
07:41:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
326.454 km
Perigee altitude
291.193 km
Semi-major axis
6,686.961 km
Eccentricity
0.00264
Inclination
97.5913°
RAAN
230.1636°
Arg. of periapsis
256.201°
True anomaly
103.92599°
Mean anomaly
103.6326°
Eccentric anomaly
103.77932°
Mean motion
3.96917 °/min
Orbital period
90.7 mins
BSTAR
0.037037
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Other satellites on launch #112 in the year 2025 (2025-05-27 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.STARLINK-34343 DEB 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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| STARLINK-34343 DEB 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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