DMSP 5D-2 F13 DEB, 40570 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F13 DEB, 40570 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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40570 intel report (Beta)
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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 shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 DMSP 5D-2 F13 DEB
1 40570U 95015ED 26019.51367844 .02638083 00000-0 21566-1 0 9993
2 40570 98.6285 111.7386 0015221 319.7550 40.2579 15.66967912565166Epoch: 2026-01-19T12:19Z
TLE epoch observation values (Epoch: 2026-01-19T12:19:41.817Z)
Latitude
0.00002°
Longitude
167.90554°
Altitude
362.869 km
Speed
7.696 km/s
True Right ascension
07h 26m 57s
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
14:47:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
374.809 km
Perigee altitude
354.283 km
Semi-major axis
6,742.683 km
Eccentricity
0.00152
Inclination
98.6285°
RAAN
111.7386°
Arg. of periapsis
319.755°
True anomaly
40.37078°
Mean anomaly
40.2579°
Eccentric anomaly
40.31432°
Mean motion
3.92007 °/min
Orbital period
91.84 mins
BSTAR
0.021566
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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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