DMSP 5D-2 F13 DEB, 42326 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F13 DEB, 42326 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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42326 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 3 weeks ago
TLE from 3 weeks ago
0 DMSP 5D-2 F13 DEB
1 42326U 95015JU 25263.24011796 .01541361 00000-0 23458-1 0 9999
2 42326 98.7497 2.3325 0020047 275.4061 84.4900 15.51505669519649
Epoch: 2025-09-20T05:45Z
TLE epoch observation values (Epoch: 2025-09-20T05:45:46.191Z)
Latitude
-0.00004°
Longitude
-83.48581°
Altitude
414.139 km
Speed
7.663 km/s
True Right ascension
00h 09m 19s
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
09:33:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
422.923 km
Perigee altitude
395.71 km
Semi-major axis
6,787.454 km
Eccentricity
0.002
Inclination
98.7497°
RAAN
2.3325°
Arg. of periapsis
275.4061°
True anomaly
84.71871°
Mean anomaly
84.49°
Eccentric anomaly
84.60435°
Mean motion
3.88135 °/min
Orbital period
92.75 mins
BSTAR
0.023458
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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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