DMSP 5D-2 F13 DEB, 40524 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F13 DEB, 40524 was space debris in SSO originally from a launch on Fri, 24 Mar 1995 UTC launched from the Air Force Western Test Range (AFWTR). 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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40524 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 DMSP 5D-2 F13 DEB
1 40524U 95015DL 24151.65369892 .00251845 00000-0 13178-1 0 9992
2 40524 98.5608 241.4193 0027030 285.4038 74.4204 15.14344088484330
Epoch: 2024-05-30T15:41Z
TLE epoch observation values (Epoch: 2024-05-30T15:41:19.586Z)
Latitude
-0.00012°
Longitude
117.44366°
Altitude
521.054 km
Speed
7.606 km/s
True Right ascension
16h 05m 40s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
12:58:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
538.643 km
Perigee altitude
501.351 km
Semi-major axis
6,898.134 km
Eccentricity
0.0027
Inclination
98.5608°
RAAN
241.4193°
Arg. of periapsis
285.4038°
True anomaly
74.71903°
Mean anomaly
74.4204°
Eccentric anomaly
74.56969°
Mean motion
3.78831 °/min
Orbital period
95.03 mins
BSTAR
0.013178
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Other satellites on launch #15 in the year 1995 (1995-03-24 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.DMSP 5D-2 F13 DEB Visibility
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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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This satellite is decayed. |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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