DMSP 5D-2 F13 DEB, 40559 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F13 DEB, 40559 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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40559 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 3 months ago
TLE from 3 months ago
0 DMSP 5D-2 F13 DEB
1 40559U 95015DS 25267.27726763 .00804922 00000-0 32235-1 0 9996
2 40559 98.5209 205.0056 0022490 130.2138 230.1068 15.22218509542760Epoch: 2025-09-24T06:39Z
TLE epoch observation values (Epoch: 2025-09-24T06:39:15.923Z)
Latitude
0.00003°
Longitude
101.83419°
Altitude
512.152 km
Speed
7.602 km/s
True Right ascension
13h 40m 01s
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
13:35:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.625 km
Perigee altitude
480.704 km
Semi-major axis
6,874.302 km
Eccentricity
0.00225
Inclination
98.5209°
RAAN
205.0056°
Arg. of periapsis
130.2138°
True anomaly
229.90943°
Mean anomaly
230.1068°
Eccentric anomaly
230.00808°
Mean motion
3.80803 °/min
Orbital period
94.54 mins
BSTAR
0.032235
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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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