BREEZE-M DEB, 43407
Orbit data source: Space-Track
BREEZE-M DEB, 43407 is space debris in HEO originally from a launch on Mon, 15 Apr 2013 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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43407 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 BREEZE-M DEB
1 43407U 13014D 25241.01063105 -.00000133 00000-0 00000-0 0 9995
2 43407 15.3722 22.3719 4833368 175.1030 192.4589 1.91517184 69769
Epoch: 2025-08-29T00:15Z
TLE epoch observation values (Epoch: 2025-08-29T00:15:18.522Z)
Latitude
-0.00003°
Longitude
41.08942°
Altitude
34,109.326 km
Speed
2.267 km/s
True Right ascension
01h 29m 31s
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
15:50:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,254.098 km
Perigee altitude
7,774.536 km
Semi-major axis
27,392.454 km
Eccentricity
0.48334
Inclination
15.3722°
RAAN
22.3719°
Arg. of periapsis
175.103°
True anomaly
184.96867°
Mean anomaly
192.4589°
Eccentric anomaly
188.40907°
Mean motion
0.47874 °/min
Orbital period
751.98 mins
BSTAR
0
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Other satellites on launch #14 in the year 2013 (2013-04-15 UTC)
BREEZE-M DEB 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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116 mins | 2025-08-31 19:04:29.258Z | 267.894° W | 2025-08-31 20:23:29.258Z | 206.169° SW | 30.733° | 2025-08-31 21:00:29.258Z | 139.871° SSE |
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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