ATLAS 5 CENTAUR DEB, 43960
Orbit data source: Space-Track
ATLAS 5 CENTAUR DEB, 43960 is space debris in HEO originally from a launch on Wed, 17 Sep 2014 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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43960 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 week ago
TLE from 1 week ago
0 ATLAS 5 CENTAUR DEB
1 43960U 14055P 25251.97676372 .00000007 00000-0 00000-0 0 9996
2 43960 19.5403 165.8513 5115551 124.0897 295.2297 1.81612472 46535Epoch: 2025-09-08T23:26Z
TLE epoch observation values (Epoch: 2025-09-08T23:26:32.385Z)
Latitude
0.00002°
Longitude
-174.11327°
Altitude
23,046.299 km
Speed
3.612 km/s
True Right ascension
11h 03m 10s
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
12:45:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,518.851 km
Perigee altitude
7,483.624 km
Semi-major axis
28,379.375 km
Eccentricity
0.51156
Inclination
19.5403°
RAAN
165.8513°
Arg. of periapsis
124.0897°
True anomaly
235.84837°
Mean anomaly
295.2297°
Eccentric anomaly
265.99145°
Mean motion
0.45398 °/min
Orbital period
792.98 mins
BSTAR
0
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Other satellites on launch #55 in the year 2014 (2014-09-17 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.ATLAS 5 CENTAUR DEB Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 61 mins | 2025-09-17 19:57:54.972Z | 168.365° S | 2025-09-17 20:04:54.972Z | 161.485° S | 37.211° | 2025-09-17 20:58:54.972Z | 94.934° ESE |
| 452 mins | 2025-09-18 12:25:54.972Z | 218.085° SW | 2025-09-18 16:06:54.972Z | 214.343° SW | 16.095° | 2025-09-18 19:57:54.972Z | 234.629° WSW |
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 ascending 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 ascending order |
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