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 (13 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: 5 days ago

TLE from 5 days ago
0 ATLAS 5 CENTAUR R/B
1 39475U 13072P   26154.63772410  .00006060  00000-0  39792-3 0  9994
2 39475 120.4291  71.4959 0172245 252.1197 106.1013 14.97926437112549
Epoch: 2026-06-03T15:18Z
TLE epoch observation values (Epoch: 2026-06-03T15:18:19.362Z)
Latitude
-0.00005°
Longitude
-50.17822°
Altitude
609.942 km
Speed
7.536 km/s
True Right ascension
04h 45m 59s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
11:27:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
692.301 km
Perigee altitude
452.856 km
Semi-major axis
6,950.715 km
Eccentricity
0.01722
Inclination
120.4291°
RAAN
71.4959°
Arg. of periapsis
252.1197°
True anomaly
107.98606°
Mean anomaly
106.1013°
Eccentric anomaly
107.04484°
Mean motion
3.74541 °/min
Orbital period
96.12 mins
BSTAR
0.00039792
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