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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24675 intel report (Beta)
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Edit Public Description
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
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
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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Other satellites on launch #70 in the year 1996 (1996-12-18 UTC)
ATLAS 2A CENTAUR R/B Visibility forecast
Observer location: undefined°, undefined°
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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301 mins | 2025-08-02 22:21:05.660Z | 109.941° ESE | 2025-08-03 02:06:05.660Z | 114.812° SE | 28.345° | 2025-08-03 03:22:05.660Z | 90.148° ESE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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