DMSP 5D-2 F13 DEB, 40579 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F13 DEB, 40579 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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40579 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 DMSP 5D-2 F13 DEB
1 40579U 95015EN 26020.72824737 .02786930 00000-0 31528-1 0 9990
2 40579 98.4464 119.2292 0020662 304.7625 55.1683 15.58832449569301Epoch: 2026-01-20T17:28Z
TLE epoch observation values (Epoch: 2026-01-20T17:28:40.572Z)
Latitude
0.00001°
Longitude
96.95419°
Altitude
386.175 km
Speed
7.683 km/s
True Right ascension
07h 56m 55s
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
15:38:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
401.978 km
Perigee altitude
374.017 km
Semi-major axis
6,766.135 km
Eccentricity
0.00207
Inclination
98.4464°
RAAN
119.2292°
Arg. of periapsis
304.7625°
True anomaly
55.36293°
Mean anomaly
55.1683°
Eccentric anomaly
55.26559°
Mean motion
3.89971 °/min
Orbital period
92.31 mins
BSTAR
0.031528
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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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