DMSP 5D-2 F11 DEB, 29073 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F11 DEB, 29073 was space debris in SSO originally from a launch on Thu, 28 Nov 1991 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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29073 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 8 months ago
TLE from 8 months ago
0 DMSP 5D-2 F11 DEB
1 29073U 91082BU 25107.77730120 .00730195 00000-0 15246-1 0 9997
2 29073 98.5216 218.4695 0018658 267.7625 92.1483 15.42993483620869Epoch: 2025-04-17T18:39Z
TLE epoch observation values (Epoch: 2025-04-17T18:39:18.823Z)
Latitude
-0.00001°
Longitude
92.49674°
Altitude
440.868 km
Speed
7.647 km/s
True Right ascension
14h 33m 52s
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
19:51:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
446.978 km
Perigee altitude
421.557 km
Semi-major axis
6,812.404 km
Eccentricity
0.00187
Inclination
98.5216°
RAAN
218.4695°
Arg. of periapsis
267.7625°
True anomaly
92.36194°
Mean anomaly
92.1483°
Eccentric anomaly
92.25512°
Mean motion
3.86005 °/min
Orbital period
93.26 mins
BSTAR
0.015246
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Other satellites on launch #82 in the year 1991 (1991-11-28 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 F11 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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