DMSP 5D-2 F13 DEB, 42279
Orbit data source: Space-Track
DMSP 5D-2 F13 DEB, 42279 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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42279 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 4 weeks ago
TLE from 4 weeks ago
0 DMSP 5D-2 F13 DEB
1 42279U 95015GV 26094.46774113 .00851204 00000-0 21006-1 0 9998
2 42279 98.7146 182.3284 0014650 263.6856 96.2716 15.37964958571978Epoch: 2026-04-04T11:13Z
TLE epoch observation values (Epoch: 2026-04-04T11:13:32.833Z)
Latitude
-0.00007°
Longitude
-178.84549°
Altitude
456.309 km
Speed
7.638 km/s
True Right ascension
12h 09m 18s
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
16:43:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.133 km
Perigee altitude
439.129 km
Semi-major axis
6,827.268 km
Eccentricity
0.00147
Inclination
98.7146°
RAAN
182.3284°
Arg. of periapsis
263.6856°
True anomaly
96.43844°
Mean anomaly
96.2716°
Eccentric anomaly
96.35502°
Mean motion
3.84745 °/min
Orbital period
93.57 mins
BSTAR
0.021006
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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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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