BREEZE-M DEB, 38960 (Decayed)
Orbit data source: Space-Track
BREEZE-M DEB, 38960 was space debris in LEO originally from a launch on Mon, 06 Aug 2012 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). 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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38960 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Khrunichev
Mission
Decayed spacecraft
Bus & Motor
BRIZ, Unknown motor
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 9 months ago
TLE from 9 months ago
0 BREEZE-M DEB
1 38960U 12044CT 25250.91128396 .06095475 11669-4 94205-3 0 9996
2 38960 49.9901 50.8138 0051197 213.4474 146.3288 16.28879601508376Epoch: 2025-09-07T21:52Z
TLE epoch observation values (Epoch: 2025-09-07T21:52:14.934Z)
Latitude
0.00002°
Longitude
95.52762°
Altitude
224.19 km
Speed
7.757 km/s
True Right ascension
03h 23m 15s
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
00:39:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
230.02 km
Perigee altitude
162.701 km
Semi-major axis
6,574.498 km
Eccentricity
0.00512
Inclination
49.9901°
RAAN
50.8138°
Arg. of periapsis
213.4474°
True anomaly
146.65234°
Mean anomaly
146.3288°
Eccentric anomaly
146.49074°
Mean motion
4.07145 °/min
Orbital period
88.42 mins
BSTAR
0.00094205
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Other satellites on launch #44 in the year 2012 (2012-08-06 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.BREEZE-M 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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| This satellite is decayed. |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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