DMSP 5D-2 F13 DEB, 40475 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F13 DEB, 40475 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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40475 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 10 months ago
TLE from 10 months ago
0 DMSP 5D-2 F13 DEB
1 40475U 95015BT 24314.82187157 .00132684 00000-0 42294-1 0 9999
2 40475 98.9540 326.6159 0034606 264.6181 95.1056 14.38496530498499
Epoch: 2024-11-09T19:43Z
TLE epoch observation values (Epoch: 2024-11-09T19:43:29.703Z)
Latitude
-0.00007°
Longitude
-18.72818°
Altitude
768.687 km
Speed
7.469 km/s
True Right ascension
21h 46m 27s
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
13:34:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
785.32 km
Perigee altitude
735.912 km
Semi-major axis
7,138.753 km
Eccentricity
0.00346
Inclination
98.954°
RAAN
326.6159°
Arg. of periapsis
264.6181°
True anomaly
95.50043°
Mean anomaly
95.1056°
Eccentric anomaly
95.30303°
Mean motion
3.5984 °/min
Orbital period
100.04 mins
BSTAR
0.042294
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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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