ATLAS 5 CENTAUR R/B, 39207

Orbit data source: Space-Track

ATLAS 5 CENTAUR R/B, 39207 is space debris in HEO originally from a launch on Fri, 19 Jul 2013 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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Identifier
39207, 2013-036B
Orbit
HEO
Last TLE update
2 days ago
Origin
Manufacturer
LMSS Denver
Mission
Spacecraft
Bus & Motor
CENTAUR SEC, RL10-4A-2
Mass
~2,020 kg wet, 2,020 kg dry
Launch date (UTC)
2013-07-19 (12 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 5.8 m
Radar Cross Section
32.260 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 2 days ago
0 ATLAS 5 CENTAUR R/B
1 39207U 13036B   25212.62549640 -.00000169  00000-0  00000-0 0  9999
2 39207  17.5173 218.0977 6172511 255.0884  32.6204  2.09947577 92318
Epoch: 2025-07-31T15:00Z
TLE epoch observation values (Epoch: 2025-07-31T15:00:42.888Z)
Latitude
-0.00016°
Longitude
43.37748°
Altitude
12,542.968 km
Speed
5.163 km/s
True Right ascension
14h 32m 10s
True Declination
0° 00' 01"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
16.65183°
Longitude
114.36252°
Altitude
35,161.285 km
Speed
1.929 km/s
Apparent Right ascension
19h 12m 58s
Apparent Declination
9° 55' 55"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
06:47:22
Azimuth
351.784° N
Elevation
-39.8°
Doppler factor
1
Orbital elements
Apogee altitude
35,291.858 km
Perigee altitude
3,483.748 km
Semi-major axis
25,765.94 km
Eccentricity
0.61725
Inclination
17.5173°
RAAN
218.0977°
Arg. of periapsis
255.0884°
True anomaly
104.79337°
Mean anomaly
32.6204°
Eccentric anomaly
64.55599°
Mean motion
0.52478 °/min
Orbital period
686.01 mins
BSTAR
0
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