ATLAS 5 CENTAUR DEB, 43984

Orbit data source: Space-Track

ATLAS 5 CENTAUR DEB, 43984 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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Identifier
43984, 2014-055AP
Orbit
HEO
Last TLE update
1 week ago
Origin
Flag of USUnited Launch Alliance/Lockheed Martin (US)
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2014-09-17 (11 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history

TLE from 1 week ago
0 ATLAS 5 CENTAUR DEB
1 43984U 14055AP  25193.02718778 -.00000114  00000-0  00000-0 0  9990
2 43984  20.7045 129.3678 5105072 188.4803 157.6845  1.91691392 47903
Epoch: 2025-07-12T00:39Z
TLE epoch observation values (Epoch: 2025-07-12T00:39:09.024Z)
Latitude
0.00004°
Longitude
-170.62317°
Altitude
34,529.078 km
Speed
2.22 km/s
True Right ascension
08h 37m 20s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
16.86824°
Longitude
-118.21556°
Altitude
25,227.845 km
Speed
3.266 km/s
Apparent Right ascension
12h 02m 53s
Apparent Declination
11° 20' 22"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
12:28:07
Azimuth
192.795° SSW
Elevation
60.882°
Doppler factor
1
Orbital elements
Apogee altitude
34,973.159 km
Perigee altitude
7,022.105 km
Semi-major axis
27,375.769 km
Eccentricity
0.51051
Inclination
20.7045°
RAAN
129.3678°
Arg. of periapsis
188.4803°
True anomaly
171.5263°
Mean anomaly
157.6845°
Eccentric anomaly
165.17072°
Mean motion
0.47917 °/min
Orbital period
751.29 mins
BSTAR
0
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