DMSP 5D-2 F13 DEB, 42324 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F13 DEB, 42324 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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42324 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 42324U 95015JS 25027.14448995 .00405959 00000-0 21182-1 0 9992
2 42324 98.7380 106.4363 0007408 285.6771 74.3639 15.13938366485521
Epoch: 2025-01-27T03:28Z
TLE epoch observation values (Epoch: 2025-01-27T03:28:03.931Z)
Latitude
-0.00006°
Longitude
-72.24889°
Altitude
525.869 km
Speed
7.601 km/s
True Right ascension
07h 05m 44s
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
02:45:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
526.35 km
Perigee altitude
516.128 km
Semi-major axis
6,899.376 km
Eccentricity
0.00074
Inclination
98.738°
RAAN
106.4363°
Arg. of periapsis
285.6771°
True anomaly
74.44567°
Mean anomaly
74.3639°
Eccentric anomaly
74.40478°
Mean motion
3.78729 °/min
Orbital period
95.05 mins
BSTAR
0.021182
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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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