DMSP 5D-2 F13 DEB, 40495 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F13 DEB, 40495 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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40495 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 40495U 95015CJ 25078.53076680 .02037170 00000-0 36223-1 0 9996
2 40495 98.5342 193.4504 0018569 263.2824 96.6309 15.46696102527396
Epoch: 2025-03-19T12:44Z
TLE epoch observation values (Epoch: 2025-03-19T12:44:18.251Z)
Latitude
-0.00002°
Longitude
-174.94321°
Altitude
430.973 km
Speed
7.652 km/s
True Right ascension
12h 53m 48s
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
14:08:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
436.011 km
Perigee altitude
410.752 km
Semi-major axis
6,801.519 km
Eccentricity
0.00186
Inclination
98.5342°
RAAN
193.4504°
Arg. of periapsis
263.2824°
True anomaly
96.8422°
Mean anomaly
96.6309°
Eccentric anomaly
96.73656°
Mean motion
3.86932 °/min
Orbital period
93.04 mins
BSTAR
0.036223
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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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