USA 142 DEB, 25675 (Decayed)
Orbit data source: Space-Track
USA 142 DEB, 25675 was space debris in LEO originally from a launch on Fri, 09 Apr 1999 UTC launched from the Air Force Eastern Test Range (AFETR). 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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25675 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Boeing/Kent
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.3 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 3 months ago
TLE from 3 months ago
0 USA 142 DEB
1 25675U 99017E 26072.28877355 .06560405 -59502-5 90766-2 0 9996
2 25675 28.8598 55.8282 0561827 213.5089 142.8731 14.97008536130412Epoch: 2026-03-13T06:55Z
TLE epoch observation values (Epoch: 2026-03-13T06:55:50.034Z)
Latitude
0.00001°
Longitude
140.94329°
Altitude
893.348 km
Speed
7.237 km/s
True Right ascension
03h 43m 18s
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
23:07:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
971.234 km
Perigee altitude
189.348 km
Semi-major axis
6,958.428 km
Eccentricity
0.05618
Inclination
28.8598°
RAAN
55.8282°
Arg. of periapsis
213.5089°
True anomaly
146.55005°
Mean anomaly
142.8731°
Eccentric anomaly
144.73178°
Mean motion
3.73918 °/min
Orbital period
96.28 mins
BSTAR
0.0090766
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Other satellites on launch #17 in the year 1999 (1999-04-09 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.USA 142 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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