DMSP 5D-2 F13 DEB, 40481 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F13 DEB, 40481 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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40481 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 5 months ago
TLE from 5 months ago
0 DMSP 5D-2 F13 DEB
1 40481U 95015BZ 25110.88168360 .00297793 00000-0 19319-1 0 9997
2 40481 98.5623 83.1741 0022086 86.7552 273.6199 15.06388858522544Epoch: 2025-04-20T21:09Z
TLE epoch observation values (Epoch: 2025-04-20T21:09:37.463Z)
Latitude
0.00004°
Longitude
-83.43616°
Altitude
549.35 km
Speed
7.588 km/s
True Right ascension
05h 32m 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
10:40:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
559.571 km
Perigee altitude
528.994 km
Semi-major axis
6,922.42 km
Eccentricity
0.00221
Inclination
98.5623°
RAAN
83.1741°
Arg. of periapsis
86.7552°
True anomaly
273.36727°
Mean anomaly
273.6199°
Eccentric anomaly
273.49359°
Mean motion
3.76839 °/min
Orbital period
95.53 mins
BSTAR
0.019319
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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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