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)
DMSP 5D-2 F13 DEB details
Identifier | |
Orbit | Decayed |
Last TLE update | 7 months ago |
Origin | |
Manufacturer | Unknown |
Mission | Decayed spacecraft |
Bus & Motor | Unknown |
Mass | Unknown |
Launch date (UTC) | |
Launch vehicle | Unknown |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Unknown |
Radar Cross Section | Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 7 months 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
Definitive object data (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 | Object was in full shadow at TLE epoch |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Orbital elements
Apogee altitude | 538.643 km |
Perigee altitude | 501.351 km |
Semi-major axis | 6,898.134 km |
Eccentricity | 0.002703 |
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 |
BSTAR | 0.013178 |
Orbital period | 95.03 mins |
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Other satellites on launch #15 in the year 1995 (1995-03-24 UTC)
DMSP 5D-2 F13 DEB Visibility forecast
Observer location: undefined°, undefined
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