ATLAS 5 CENTAUR DEB, 46846
Orbit data source: Space-Track
ATLAS 5 CENTAUR DEB, 46846 is space debris in HEO originally from a launch on Wed, 17 Oct 2018 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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46846 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 2 weeks ago
0 ATLAS 5 CENTAUR DEB
1 46846U 18079DB 25188.46753150 -.00000132 00000-0 00000-0 0 9995
2 46846 11.6912 88.5947 4590728 214.5966 104.3817 1.71772081 29378
Epoch: 2025-07-07T11:13Z
TLE epoch observation values (Epoch: 2025-07-07T11:13:14.721Z)
Latitude
0.00001°
Longitude
-5.42614°
Altitude
31,011.111 km
Speed
2.791 km/s
True Right ascension
05h 54m 14s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
-4.35741°
Longitude
-27.76943°
Altitude
24,267.728 km
Speed
3.533 km/s
Apparent Right ascension
04h 28m 35s
Apparent Declination
-13° 59' 10"
Sunlit
Visualization observer readout
Local Sidereal Time
04:05:23
Azimuth
173.057° S
Elevation
35.828°
Doppler factor
1
Orbital elements
Apogee altitude
36,595.97 km
Perigee altitude
9,553.805 km
Semi-major axis
29,453.025 km
Eccentricity
0.45907
Inclination
11.6912°
RAAN
88.5947°
Arg. of periapsis
214.5966°
True anomaly
145.34121°
Mean anomaly
104.3817°
Eccentric anomaly
125.73303°
Mean motion
0.42939 °/min
Orbital period
838.41 mins
BSTAR
0
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Other satellites on launch #79 in the year 2018 (2018-10-17 UTC)
ATLAS 5 CENTAUR DEB 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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651 mins | 2025-07-19 15:15:11.418Z | 173.06° S | 2025-07-19 23:49:11.418Z | 198.621° SSW | 38.857° | 2025-07-20 02:06:11.418Z | 122.643° SE |
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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