ATLAS 5 CENTAUR R/B, 39475

Orbit data source: Space-Track

ATLAS 5 CENTAUR R/B, 39475 is space debris in LEO originally from an American launch on Fri, 06 Dec 2013 UTC via an ATLAS V 501 launch vehicle 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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Identifier
39475, 2013-072P
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
USN PGS
Mission
Spacecraft
Bus & Motor
NPSCUL, Unknown motor
Mass
~45 kg wet, ~45 kg dry
Launch date (UTC)
2013-12-06 (12 years ago)
Launch vehicle
ATLAS V 501
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + Box + 1 Nozzle, 6.1 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 ATLAS 5 CENTAUR R/B
1 39475U 13072P   26095.21922457  .00013710  00000-0  85654-3 0  9998
2 39475 120.4294 209.6555 0182892 188.1447 171.6625 14.97064172103640
Epoch: 2026-04-05T05:15Z
TLE epoch observation values (Epoch: 2026-04-05T05:15:41.002Z)
Latitude
-0.00006°
Longitude
-62.79309°
Altitude
703.407 km
Speed
7.437 km/s
True Right ascension
13h 58m 37s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
19:25:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
702.419 km
Perigee altitude
448.076 km
Semi-major axis
6,953.384 km
Eccentricity
0.01829
Inclination
120.4294°
RAAN
209.6555°
Arg. of periapsis
188.1447°
True anomaly
171.95967°
Mean anomaly
171.6625°
Eccentric anomaly
171.81175°
Mean motion
3.74325 °/min
Orbital period
96.17 mins
BSTAR
0.00085654
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