ATLAS 2A CENTAUR R/B, 24675

Orbit data source: Space-Track

ATLAS 2A CENTAUR R/B, 24675 is space debris in HEO originally from a launch on Wed, 18 Dec 1996 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
24675, 1996-070B
Orbit
HEO
Last TLE update
1 day ago
Origin
Manufacturer
LMA/DENV
Mission
Spacecraft
Bus & Motor
CENTAUR, Unknown motor
Mass
2,095 kg wet, 2,095 kg dry
Launch date (UTC)
1996-12-18 (29 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 5.0 m
Radar Cross Section
27.847 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago
0 ATLAS 2A CENTAUR R/B
1 24675U 96070B   25213.36494024 -.00000037  00000-0  00000-0 0  9992
2 24675  22.4857 251.0121 7010662 175.8617 352.9721  2.22634425232795
Epoch: 2025-08-01T08:45Z
TLE epoch observation values (Epoch: 2025-08-01T08:45:30.836Z)
Latitude
18.30081°
Longitude
-63.4098°
Altitude
2,365.287 km
Speed
8.666 km/s
True Right ascension
01h 12m 44s
True Declination
18° 13' 02"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
5.42334°
Longitude
-177.65565°
Altitude
31,519.57 km
Speed
2.224 km/s
Apparent Right ascension
17h 22m 58s
Apparent Declination
0° 40' 16"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
03:41:16
Azimuth
323.04° NNW
Elevation
-44.441°
Doppler factor
1
Orbital elements
Apogee altitude
35,771.664 km
Perigee altitude
1,028.982 km
Semi-major axis
24,778.46 km
Eccentricity
0.70107
Inclination
22.4857°
RAAN
251.0121°
Arg. of periapsis
175.8617°
True anomaly
309.81061°
Mean anomaly
352.9721°
Eccentric anomaly
337.78558°
Mean motion
0.55646 °/min
Orbital period
646.95 mins
BSTAR
0
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