DMSP 5D-2 F13 DEB, 40438
Orbit data source: Space-Track
DMSP 5D-2 F13 DEB, 40438 is 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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40438 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 2 weeks ago
TLE from 2 weeks ago
0 DMSP 5D-2 F13 DEB
1 40438U 95015AQ 26020.00418479 .01803866 00000-0 46086-1 0 9999
2 40438 98.8371 87.0709 0005218 279.5227 80.5423 15.36159575566330Epoch: 2026-01-20T00:06Z
TLE epoch observation values (Epoch: 2026-01-20T00:06:01.565Z)
Latitude
-0.00001°
Longitude
-33.8279°
Altitude
459.961 km
Speed
7.637 km/s
True Right ascension
05h 48m 17s
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
22:57:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
458.055 km
Perigee altitude
450.925 km
Semi-major axis
6,832.627 km
Eccentricity
0.00052
Inclination
98.8371°
RAAN
87.0709°
Arg. of periapsis
279.5227°
True anomaly
80.60129°
Mean anomaly
80.5423°
Eccentric anomaly
80.57179°
Mean motion
3.84292 °/min
Orbital period
93.68 mins
BSTAR
0.046086
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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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| DMSP 5D-2 F13 DEB is likely not visible in the next few days. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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