DMSP 5D-2 F13 DEB, 42329 (Decayed)
Orbit data source: Space-Track
DMSP 5D-2 F13 DEB, 42329 was space debris in SSO originally from a launch on Fri, 24 Mar 1995 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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42329 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
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 DMSP 5D-2 F13 DEB
1 42329U 95015JX 24224.97830317 .00103400 00000-0 16989-1 0 9994
2 42329 98.5432 306.7124 0046746 128.9840 231.5542 14.69299344 9175Epoch: 2024-08-11T23:28Z
TLE epoch observation values (Epoch: 2024-08-11T23:28:45.393Z)
Latitude
-0.00007°
Longitude
-6.39298°
Altitude
686.857 km
Speed
7.502 km/s
True Right ascension
20h 26m 50s
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
19:47:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
693.293 km
Perigee altitude
627.488 km
Semi-major axis
7,038.528 km
Eccentricity
0.00467
Inclination
98.5432°
RAAN
306.7124°
Arg. of periapsis
128.984°
True anomaly
231.13619°
Mean anomaly
231.5542°
Eccentric anomaly
231.34504°
Mean motion
3.67553 °/min
Orbital period
97.94 mins
BSTAR
0.016989
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Other satellites on launch #15 in the year 1995 (1995-03-24 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 F13 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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