NOAA 16 DEB, 41519 (Decayed)
Orbit data source: Space-Track
NOAA 16 DEB, 41519 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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41519 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 months ago
TLE from 3 months ago
0 NOAA 16 DEB
1 41519U 00055MT 25192.18492352 .01115139 00000-0 13080-1 0 9997
2 41519 98.7867 339.0083 0027334 287.1523 72.6736 15.58491126480184Epoch: 2025-07-11T04:26Z
TLE epoch observation values (Epoch: 2025-07-11T04:26:17.392Z)
Latitude
-0.00001°
Longitude
-16.90465°
Altitude
389.656 km
Speed
7.679 km/s
True Right ascension
22h 36m 01s
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
17:14:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
407.501 km
Perigee altitude
370.506 km
Semi-major axis
6,767.141 km
Eccentricity
0.00273
Inclination
98.7867°
RAAN
339.0083°
Arg. of periapsis
287.1523°
True anomaly
72.97291°
Mean anomaly
72.6736°
Eccentric anomaly
72.82323°
Mean motion
3.89884 °/min
Orbital period
92.34 mins
BSTAR
0.01308
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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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