DMSP 5D-2 F13 DEB, 42317 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F13 DEB, 42317 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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42317 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 8 months ago
TLE from 8 months ago
0 DMSP 5D-2 F13 DEB
1 42317U 95015JK 25052.80216932 .00818418 00000-0 27379-1 0 9991
2 42317 98.7137 156.1729 0013719 286.5074 73.4654 15.28328947498951
Epoch: 2025-02-21T19:15Z
TLE epoch observation values (Epoch: 2025-02-21T19:15:07.429Z)
Latitude
-0.00002°
Longitude
75.43371°
Altitude
481.202 km
Speed
7.626 km/s
True Right ascension
10h 24m 41s
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
23:11:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
487.229 km
Perigee altitude
468.417 km
Semi-major axis
6,855.96 km
Eccentricity
0.00137
Inclination
98.7137°
RAAN
156.1729°
Arg. of periapsis
286.5074°
True anomaly
73.61618°
Mean anomaly
73.4654°
Eccentric anomaly
73.54078°
Mean motion
3.82332 °/min
Orbital period
94.16 mins
BSTAR
0.027379
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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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