DMSP 5D-2 F14 DEB, 62935 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F14 DEB, 62935 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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62935 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 DMSP 5D-2 F14 DEB
1 62935U 97012F 25090.13758942 .24319656 00000-0 19860+0 0 9998
2 62935 98.8900 145.6424 0025388 274.9105 84.9251 15.64760549 14754Epoch: 2025-03-31T03:18Z
TLE epoch observation values (Epoch: 2025-03-31T03:18:07.725Z)
Latitude
-0.00006°
Longitude
-92.64758°
Altitude
375.557 km
Speed
7.685 km/s
True Right ascension
09h 42m 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
07:14:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
388.039 km
Perigee altitude
353.77 km
Semi-major axis
6,749.042 km
Eccentricity
0.00254
Inclination
98.89°
RAAN
145.6424°
Arg. of periapsis
274.9105°
True anomaly
85.21496°
Mean anomaly
84.9251°
Eccentric anomaly
85.07002°
Mean motion
3.91453 °/min
Orbital period
91.96 mins
BSTAR
0.1986
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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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