ATLAS V CENTAUR R/B, 41329

Orbit data source: Space-Track

ATLAS V CENTAUR R/B, 41329 is space debris in MEO originally from a launch on Fri, 05 Feb 2016 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
41329, 2016-007B
Orbit
MEO
Country
Flag of USUS
Related business
Flag of USUnited Launch Alliance/Lockheed Martin (US)
Manufacturer
LMSS Denver
Mission
Spacecraft
Bus & Motor
CENTAUR SEC, RL10C-1
Mass
~2,020 kg wet, 2,020 kg dry
Launch date (UTC)
2016-02-05 (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
Last TLE update: 1 day ago

TLE from 1 day ago
0 ATLAS V CENTAUR R/B
1 41329U 16007B   25311.79914981  .00000042  00000-0  00000-0 0  9999
2 41329  55.5980 111.8788 0110785 352.5148   7.3131  1.91799299 68361
Epoch: 2025-11-07T19:10Z
TLE epoch observation values (Epoch: 2025-11-07T19:10:46.543Z)
Latitude
Longitude
136.9278°
Altitude
20,684.97 km
Speed
3.859 km/s
True Right ascension
07h 27m 26s
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
17:28:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
21,288.419 km
Perigee altitude
20,682.128 km
Semi-major axis
27,363.41 km
Eccentricity
0.01108
Inclination
55.598°
RAAN
111.8788°
Arg. of periapsis
352.5148°
True anomaly
7.47695°
Mean anomaly
7.3131°
Eccentric anomaly
7.3948°
Mean motion
0.4795 °/min
Orbital period
750.78 mins
BSTAR
0
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Other satellites on launch #7 in the year 2016 (2016-02-05 UTC)

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