ATLAS 5 CENTAUR DEB, 43966

Orbit data source: Space-Track

ATLAS 5 CENTAUR DEB, 43966 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.

Loading next visibility...
Identifier
43966, 2014-055V
Orbit
HEO
Country
Flag of USUS
Related business
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 shape, 1.1 m
Radar Cross Section
Small (<0.1 m²)

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

TLE from 8 months ago
0 ATLAS 5 CENTAUR DEB
1 43966U 14055V   25045.51738254 -.00000021  00000-0  00000-0 0  9998
2 43966  19.4937 182.2211 5157195  95.9599 322.3502  1.83013172 43122
Epoch: 2025-02-14T12:25Z
TLE epoch observation values (Epoch: 2025-02-14T12:25:01.851Z)
Latitude
-0.00001°
Longitude
-148.93848°
Altitude
15,559.373 km
Speed
4.714 km/s
True Right ascension
12h 08m 23s
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
23:17:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,417.336 km
Perigee altitude
7,295.246 km
Semi-major axis
28,234.428 km
Eccentricity
0.51572
Inclination
19.4937°
RAAN
182.2211°
Arg. of periapsis
95.9599°
True anomaly
263.96761°
Mean anomaly
322.3502°
Eccentric anomaly
295.73179°
Mean motion
0.45748 °/min
Orbital period
786.91 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|