NOAA 16 DEB, 42352 (Decayed)
Orbit data source: Space-Track
NOAA 16 DEB, 42352 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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42352 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: 3 weeks ago
TLE from 3 weeks ago
0 NOAA 16 DEB
1 42352U 00055QU 26016.02543853 .06210316 00000-0 22471-1 0 9997
2 42352 98.8999 196.8747 0015306 333.4933 26.5547 15.84516113509586Epoch: 2026-01-16T00:36Z
TLE epoch observation values (Epoch: 2026-01-16T00:36:37.888Z)
Latitude
-0.00013°
Longitude
72.24621°
Altitude
311.65 km
Speed
7.726 km/s
True Right ascension
13h 07m 29s
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
13:12:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
324.884 km
Perigee altitude
304.396 km
Semi-major axis
6,692.777 km
Eccentricity
0.00153
Inclination
98.8999°
RAAN
196.8747°
Arg. of periapsis
333.4933°
True anomaly
26.63324°
Mean anomaly
26.5547°
Eccentric anomaly
26.59396°
Mean motion
3.964 °/min
Orbital period
90.82 mins
BSTAR
0.022471
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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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