ATLAS 5 CENTAUR R/B, 40731
Orbit data source: Space-Track
ATLAS 5 CENTAUR R/B, 40731 is space debris in MEO originally from a launch on Wed, 15 Jul 2015 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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40731 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 1 day ago
0 ATLAS 5 CENTAUR R/B
1 40731U 15033B 25198.73234961 -.00000057 00000-0 00000-0 0 9990
2 40731 54.8648 296.3303 0230661 4.1926 356.0363 1.90866757 69761
Epoch: 2025-07-17T17:34Z
TLE epoch observation values (Epoch: 2025-07-17T17:34:35.006Z)
Latitude
0°
Longitude
96.88778°
Altitude
20,442.153 km
Speed
3.899 km/s
True Right ascension
19h 45m 18s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
35.95418°
Longitude
-113.77843°
Altitude
21,476.064 km
Speed
3.756 km/s
Apparent Right ascension
04h 54m 59s
Apparent Declination
27° 27' 56"
Sunlit
Visualization observer readout
Local Sidereal Time
12:07:27
Azimuth
302.186° NW
Elevation
4.838°
Doppler factor
1
Orbital elements
Apogee altitude
21,707.581 km
Perigee altitude
20,441.137 km
Semi-major axis
27,452.496 km
Eccentricity
0.02307
Inclination
54.8648°
RAAN
296.3303°
Arg. of periapsis
4.1926°
True anomaly
355.84819°
Mean anomaly
356.0363°
Eccentric anomaly
355.94279°
Mean motion
0.47717 °/min
Orbital period
754.45 mins
BSTAR
0
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Other satellites on launch #33 in the year 2015 (2015-07-15 UTC)
ATLAS 5 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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377 mins | 2025-07-19 06:13:51.873Z | 188.952° SSW | 2025-07-19 08:57:51.873Z | 112.073° ESE | 44.926° | 2025-07-19 12:30:51.873Z | 78.316° E |
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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