DMSP 5D-2 F11 DEB, 29090 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F11 DEB, 29090 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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29090 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 9 months ago
TLE from 9 months ago
0 DMSP 5D-2 F11 DEB
1 29090U 91082CK 25089.26771849 .00929769 00000-0 19105-1 0 9997
2 29090 98.6156 202.1481 0024418 282.0926 77.7582 15.43171458 87193Epoch: 2025-03-30T06:25Z
TLE epoch observation values (Epoch: 2025-03-30T06:25:30.877Z)
Latitude
-0.00004°
Longitude
-82.13096°
Altitude
436.35 km
Speed
7.652 km/s
True Right ascension
13h 28m 35s
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
19:52:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
450.381 km
Perigee altitude
417.114 km
Semi-major axis
6,811.885 km
Eccentricity
0.00244
Inclination
98.6156°
RAAN
202.1481°
Arg. of periapsis
282.0926°
True anomaly
78.03182°
Mean anomaly
77.7582°
Eccentric anomaly
77.89499°
Mean motion
3.86049 °/min
Orbital period
93.25 mins
BSTAR
0.019105
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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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