NOAA 16 DEB, 42392 (Decayed)
Orbit data source: Space-Track
NOAA 16 DEB, 42392 was space debris in SSO originally from a launch on Thu, 21 Sep 2000 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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42392 intel report (Beta)
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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: 1 month ago
TLE from 1 month ago
0 NOAA 16 DEB
1 42392U 00055SL 26045.44179696 .01367886 00000-0 18594-1 0 9990
2 42392 98.9262 285.1004 0010968 59.9455 300.2881 15.54648005518520Epoch: 2026-02-14T10:36Z
TLE epoch observation values (Epoch: 2026-02-14T10:36:11.257Z)
Latitude
0.00004°
Longitude
-18.41131°
Altitude
402.519 km
Speed
7.671 km/s
True Right ascension
19h 00m 24s
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
15:42:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
407.603 km
Perigee altitude
392.734 km
Semi-major axis
6,778.305 km
Eccentricity
0.0011
Inclination
98.9262°
RAAN
285.1004°
Arg. of periapsis
59.9455°
True anomaly
300.1795°
Mean anomaly
300.2881°
Eccentric anomaly
300.23381°
Mean motion
3.88921 °/min
Orbital period
92.56 mins
BSTAR
0.018594
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Other satellites on launch #55 in the year 2000 (2000-09-21 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.NOAA 16 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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