DMSP 5D-2 F13 DEB, 42293 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F13 DEB, 42293 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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42293 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 DMSP 5D-2 F13 DEB
1 42293U 95015HK 25238.80891623 .00683195 00000-0 16762-1 0 9992
2 42293 98.6887 338.8201 0020891 264.1607 95.7253 15.38194955519555
Epoch: 2025-08-26T19:24Z
TLE epoch observation values (Epoch: 2025-08-26T19:24:50.362Z)
Latitude
0.00004°
Longitude
72.31495°
Altitude
455.975 km
Speed
7.638 km/s
True Right ascension
22h 35m 16s
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
09:33:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
462.71 km
Perigee altitude
434.187 km
Semi-major axis
6,826.586 km
Eccentricity
0.00209
Inclination
98.6887°
RAAN
338.8201°
Arg. of periapsis
264.1607°
True anomaly
95.96344°
Mean anomaly
95.7253°
Eccentric anomaly
95.84437°
Mean motion
3.84802 °/min
Orbital period
93.55 mins
BSTAR
0.016762
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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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