DMSP 5D-2 F13 DEB, 40606 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F13 DEB, 40606 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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40606 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 6 months ago
TLE from 6 months ago
0 DMSP 5D-2 F13 DEB
1 40606U 95015FD 25103.44123358 .00315518 00000-0 22705-1 0 9997
2 40606 98.6890 171.9795 0011310 220.5793 139.4587 15.02519338520732
Epoch: 2025-04-13T10:35Z
TLE epoch observation values (Epoch: 2025-04-13T10:35:22.581Z)
Latitude
0.00003°
Longitude
171.26491°
Altitude
568.125 km
Speed
7.574 km/s
True Right ascension
11h 27m 55s
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
07:57:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
564.022 km
Perigee altitude
548.336 km
Semi-major axis
6,934.316 km
Eccentricity
0.00113
Inclination
98.689°
RAAN
171.9795°
Arg. of periapsis
220.5793°
True anomaly
139.54285°
Mean anomaly
139.4587°
Eccentric anomaly
139.50078°
Mean motion
3.7587 °/min
Orbital period
95.78 mins
BSTAR
0.022705
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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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