ATLAS 5 CENTAUR R/B, 40375

Orbit data source: Space-Track

ATLAS 5 CENTAUR R/B, 40375 is space debris in HEO originally from a launch on Wed, 21 Jan 2015 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
40375, 2015-002B
Orbit
HEO
Last TLE update
12 hours ago
Origin
Manufacturer
LMSS Denver
Mission
Spacecraft
Bus & Motor
CENTAUR SEC, RL10C-1
Mass
~2,020 kg wet, 2,020 kg dry
Launch date (UTC)
2015-01-21 (10 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 12 hours ago
0 ATLAS 5 CENTAUR R/B
1 40375U 15002B   25199.47426202  .00000037  00000-0  00000-0 0  9990
2 40375  19.2174 350.0337 6073948  15.7484 356.8358  2.08930276 80083
Epoch: 2025-07-18T11:22Z
TLE epoch observation values (Epoch: 2025-07-18T11:22:56.238Z)
Latitude
-0.00002°
Longitude
-117.22098°
Altitude
3,935.247 km
Speed
7.866 km/s
True Right ascension
23h 20m 09s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
17.45513°
Longitude
-53.34119°
Altitude
5,334.604 km
Speed
7.256 km/s
Apparent Right ascension
02h 34m 20s
Apparent Declination
-2° 13' 19"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
12:05:57
Azimuth
308.631° NW
Elevation
-39.507°
Doppler factor
1
Orbital elements
Apogee altitude
35,171.916 km
Perigee altitude
3,770.438 km
Semi-major axis
25,849.314 km
Eccentricity
0.60739
Inclination
19.2174°
RAAN
350.0337°
Arg. of periapsis
15.7484°
True anomaly
343.85537°
Mean anomaly
356.8358°
Eccentric anomaly
351.98097°
Mean motion
0.52224 °/min
Orbital period
689.34 mins
BSTAR
0
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