DMSP 5D-2 F14 DEB, 62947 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F14 DEB, 62947 was space debris in SSO originally from a launch on Fri, 04 Apr 1997 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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62947 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 6 months ago
TLE from 6 months ago
0 DMSP 5D-2 F14 DEB
1 62947U 97012T 25347.15309368 .07957836 00000-0 18970+0 0 9992
2 62947 99.4487 59.3958 0022547 299.1644 60.7337 15.36061668482333Epoch: 2025-12-13T03:40Z
TLE epoch observation values (Epoch: 2025-12-13T03:40:27.293Z)
Latitude
-0.00006°
Longitude
-77.80237°
Altitude
453.304 km
Speed
7.645 km/s
True Right ascension
03h 57m 34s
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
07:15:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
470.219 km
Perigee altitude
439.407 km
Semi-major axis
6,832.95 km
Eccentricity
0.00225
Inclination
99.4487°
RAAN
59.3958°
Arg. of periapsis
299.1644°
True anomaly
60.9594°
Mean anomaly
60.7337°
Eccentric anomaly
60.84652°
Mean motion
3.84265 °/min
Orbital period
93.69 mins
BSTAR
0.1897
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Other satellites on launch #12 in the year 1997 (1997-04-04 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 F14 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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