DMSP 5D-2 F11 DEB, 28338 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F11 DEB, 28338 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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28338 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 4 months ago
TLE from 4 months ago
0 DMSP 5D-2 F11 DEB
1 28338U 91082BB 25242.29092801 .02731588 00000-0 19673-1 0 9991
2 28338 98.5092 8.1780 0023843 291.3827 68.4888 15.69835400114420Epoch: 2025-08-30T06:58Z
TLE epoch observation values (Epoch: 2025-08-30T06:58:56.180Z)
Latitude
0.00005°
Longitude
-75.28343°
Altitude
356.632 km
Speed
7.699 km/s
True Right ascension
00h 32m 42s
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
11:51:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
372.376 km
Perigee altitude
340.262 km
Semi-major axis
6,734.456 km
Eccentricity
0.00238
Inclination
98.5092°
RAAN
8.178°
Arg. of periapsis
291.3827°
True anomaly
68.74327°
Mean anomaly
68.4888°
Eccentric anomaly
68.61601°
Mean motion
3.92726 °/min
Orbital period
91.67 mins
BSTAR
0.019673
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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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