ATLAS 5 CENTAUR DEB, 43954
Orbit data source: Space-Track
ATLAS 5 CENTAUR DEB, 43954 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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43954 intel report (Beta)
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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 shape, 1.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 ATLAS 5 CENTAUR DEB
1 43954U 14055H 26133.33170905 .00000028 00000-0 00000+0 0 9992
2 43954 20.5534 130.1762 4832086 191.7500 150.9035 1.89366176 53187Epoch: 2026-05-13T07:57Z
TLE epoch observation values (Epoch: 2026-05-13T07:57:39.661Z)
Latitude
0°
Longitude
139.65672°
Altitude
33,742.189 km
Speed
2.33 km/s
True Right ascension
08h 40m 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
08:53:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,557.345 km
Perigee altitude
7,884.931 km
Semi-major axis
27,599.275 km
Eccentricity
0.48321
Inclination
20.5534°
RAAN
130.1762°
Arg. of periapsis
191.75°
True anomaly
168.27009°
Mean anomaly
150.9035°
Eccentric anomaly
160.25619°
Mean motion
0.47337 °/min
Orbital period
760.51 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. |
|---|---|---|---|---|---|---|---|
| 141 mins | 2026-05-14 00:26:39.341Z | 112.456° ESE | 2026-05-14 00:43:39.341Z | 111.007° ESE | 31.459° | 2026-05-14 02:47:39.341Z | 87.473° E |
| 403 mins | 2026-05-14 17:43:39.341Z | 171.976° S | 2026-05-15 00:26:39.341Z | 139.765° SSE | 36.301° | 2026-05-15 00:26:39.341Z | 139.765° SSE |
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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