ATLAS 5 CENTAUR R/B, 39207
Orbit data source: Space-Track
ATLAS 5 CENTAUR R/B, 39207 is space debris in HEO originally from a launch on Fri, 19 Jul 2013 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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39207 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 2 days ago
0 ATLAS 5 CENTAUR R/B
1 39207U 13036B 25212.62549640 -.00000169 00000-0 00000-0 0 9999
2 39207 17.5173 218.0977 6172511 255.0884 32.6204 2.09947577 92318
Epoch: 2025-07-31T15:00Z
TLE epoch observation values (Epoch: 2025-07-31T15:00:42.888Z)
Latitude
-0.00016°
Longitude
43.37748°
Altitude
12,542.968 km
Speed
5.163 km/s
True Right ascension
14h 32m 10s
True Declination
0° 00' 01"
Sunlit
Visualization orbit readout
Latitude
16.65183°
Longitude
114.36252°
Altitude
35,161.285 km
Speed
1.929 km/s
Apparent Right ascension
19h 12m 58s
Apparent Declination
9° 55' 55"
Sunlit
Visualization observer readout
Local Sidereal Time
06:47:22
Azimuth
351.784° N
Elevation
-39.8°
Doppler factor
1
Orbital elements
Apogee altitude
35,291.858 km
Perigee altitude
3,483.748 km
Semi-major axis
25,765.94 km
Eccentricity
0.61725
Inclination
17.5173°
RAAN
218.0977°
Arg. of periapsis
255.0884°
True anomaly
104.79337°
Mean anomaly
32.6204°
Eccentric anomaly
64.55599°
Mean motion
0.52478 °/min
Orbital period
686.01 mins
BSTAR
0
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Other satellites on launch #36 in the year 2013 (2013-07-19 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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618 mins | 2025-08-02 23:39:40.615Z | 199.215° SSW | 2025-08-03 06:38:40.615Z | 167.609° S | 41.655° | 2025-08-03 09:57:40.615Z | 128.1° 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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