DMSP 5D-2 F13 DEB, 42280 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F13 DEB, 42280 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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42280 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 42280U 95015GW 25221.03694547 .07154181 66846-1 32250-1 0 9997
2 42280 98.7056 316.3680 0029055 288.6582 71.1532 15.87871010538148
Epoch: 2025-08-09T00:53Z
TLE epoch observation values (Epoch: 2025-08-09T00:53:12.088Z)
Latitude
0°
Longitude
-14.71077°
Altitude
305.166 km
Speed
7.728 km/s
True Right ascension
21h 05m 28s
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
21:04:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
324.609 km
Perigee altitude
285.773 km
Semi-major axis
6,683.328 km
Eccentricity
0.00291
Inclination
98.7056°
RAAN
316.368°
Arg. of periapsis
288.6582°
True anomaly
71.46866°
Mean anomaly
71.1532°
Eccentric anomaly
71.31089°
Mean motion
3.97241 °/min
Orbital period
90.63 mins
BSTAR
0.03225
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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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