DMSP 5D-2 F13 DEB, 40566 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F13 DEB, 40566 was space debris in LEO 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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40566 intel report (Beta)
DMSP 5D-2 F13 DEB details
Identifier | |
Orbit | Decayed |
Last TLE update | 2 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 2 months ago
0 DMSP 5D-2 F13 DEB
1 40566U 95015DZ 24277.19457528 .06478585 57290-1 37368-1 0 9999
2 40566 98.6213 56.6061 0030997 306.2039 53.6361 15.83306738501359
Epoch: 2024-10-03T04:40Z
Definitive object data (Epoch: 2024-10-03T04:40:11.304Z)
Latitude | 0° |
Longitude | -25.82409° |
Altitude | 311.961 km |
Speed | 7.728 km/s |
True Right ascension | 03h 46m 25s |
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 | 338.793 km |
Perigee altitude | 297.28 km |
Semi-major axis | 6,696.173 km |
Eccentricity | 0.0030997 |
Inclination | 98.6213° |
RAAN | 56.6061° |
Arg. of periapsis | 306.2039° |
True anomaly | 53.92279° |
Mean anomaly | 53.6361° |
Eccentric anomaly | 53.77938° |
Mean motion | 3.96098 °/min |
BSTAR | 0.037368 |
Orbital period | 90.89 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
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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