DMSP 5D-2 F13 DEB, 40431 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F13 DEB, 40431 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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40431 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: 1 year ago
TLE from 1 year ago
0 DMSP 5D-2 F13 DEB
1 40431U 95015AH 24245.23999795 .07071798 75677-1 29294-1 0 9991
2 40431 98.6100 41.4225 0027719 299.1170 60.7325 15.90325981502756Epoch: 2024-09-01T05:45Z
TLE epoch observation values (Epoch: 2024-09-01T05:45:35.822Z)
Latitude
-0.00002°
Longitude
-25.8639°
Altitude
295.502 km
Speed
7.736 km/s
True Right ascension
02h 45m 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
16:44:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
316.806 km
Perigee altitude
279.794 km
Semi-major axis
6,676.437 km
Eccentricity
0.00277
Inclination
98.61°
RAAN
41.4225°
Arg. of periapsis
299.117°
True anomaly
61.01006°
Mean anomaly
60.7325°
Eccentric anomaly
60.87123°
Mean motion
3.97856 °/min
Orbital period
90.48 mins
BSTAR
0.029294
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Other satellites on launch #15 in the year 1995 (1995-03-24 UTC)
DMSP 5D-2 F13 DEB Visibility
Observer location: undefined°, undefined°
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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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Authenticating...
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