DMSP 5D-2 F13 DEB, 42313 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F13 DEB, 42313 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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42313 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 9 months ago
TLE from 9 months ago
0 DMSP 5D-2 F13 DEB
1 42313U 95015JF 24365.11407809 .00504919 00000-0 37700-1 0 9999
2 42313 98.5252 321.1553 0019321 23.5775 336.6328 15.00418915500168
Epoch: 2024-12-30T02:44Z
TLE epoch observation values (Epoch: 2024-12-30T02:44:16.346Z)
Latitude
-0°
Longitude
-178.95352°
Altitude
556.319 km
Speed
7.59 km/s
True Right ascension
21h 24m 37s
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
21:17:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
576.057 km
Perigee altitude
549.236 km
Semi-major axis
6,940.784 km
Eccentricity
0.00193
Inclination
98.5252°
RAAN
321.1553°
Arg. of periapsis
23.5775°
True anomaly
336.54479°
Mean anomaly
336.6328°
Eccentric anomaly
336.58882°
Mean motion
3.75345 °/min
Orbital period
95.91 mins
BSTAR
0.0377
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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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