DMSP 5D-2 F13 DEB, 42270 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F13 DEB, 42270 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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42270 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 3 months ago
TLE from 3 months ago
0 DMSP 5D-2 F13 DEB
1 42270U 95015GL 25201.12204739 .00609169 00000-0 14216-1 0 9999
2 42270 98.7857 260.0175 0015384 240.1453 119.8260 15.39704618525454
Epoch: 2025-07-20T02:55Z
TLE epoch observation values (Epoch: 2025-07-20T02:55:44.894Z)
Latitude
-0.00003°
Longitude
-82.06889°
Altitude
455.291 km
Speed
7.636 km/s
True Right ascension
17h 20m 04s
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
06:51:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
454.482 km
Perigee altitude
433.491 km
Semi-major axis
6,822.124 km
Eccentricity
0.00154
Inclination
98.7857°
RAAN
260.0175°
Arg. of periapsis
240.1453°
True anomaly
119.97879°
Mean anomaly
119.826°
Eccentric anomaly
119.90241°
Mean motion
3.8518 °/min
Orbital period
93.46 mins
BSTAR
0.014216
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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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