DMSP 5D-2 F14 DEB, 62936 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F14 DEB, 62936 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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62936 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
LMT/EW
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.2 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 3 months ago
TLE from 3 months ago
0 DMSP 5D-2 F14 DEB
1 62936U 97012G 26077.96853032 .09069630 00000-0 75004-1 0 9993
2 62936 99.1975 163.4638 0027684 259.7435 100.0696 15.64661432 65675Epoch: 2026-03-18T23:14Z
TLE epoch observation values (Epoch: 2026-03-18T23:14:41.019Z)
Latitude
-0.00009°
Longitude
-1.73179°
Altitude
380.624 km
Speed
7.68 km/s
True Right ascension
10h 53m 51s
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
07:16:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
389.891 km
Perigee altitude
352.522 km
Semi-major axis
6,749.344 km
Eccentricity
0.00277
Inclination
99.1975°
RAAN
163.4638°
Arg. of periapsis
259.7435°
True anomaly
100.38176°
Mean anomaly
100.0696°
Eccentric anomaly
100.2257°
Mean motion
3.91427 °/min
Orbital period
91.97 mins
BSTAR
0.075004
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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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