NOAA 16 DEB, 41375 (Decayed)
Orbit data source: Space-Track
NOAA 16 DEB, 41375 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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41375 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: 4 months ago
TLE from 4 months ago
0 NOAA 16 DEB
1 41375U 00055JU 25163.34767279 .06532411 00000-0 26283-1 0 9996
2 41375 98.8666 0.6581 0016280 274.8895 85.0510 15.82000523487470Epoch: 2025-06-12T08:20Z
TLE epoch observation values (Epoch: 2025-06-12T08:20:38.929Z)
Latitude
-0°
Longitude
-25.42123°
Altitude
326.987 km
Speed
7.713 km/s
True Right ascension
00h 02m 37s
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
13:22:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
332.645 km
Perigee altitude
310.831 km
Semi-major axis
6,699.875 km
Eccentricity
0.00163
Inclination
98.8666°
RAAN
0.6581°
Arg. of periapsis
274.8895°
True anomaly
85.23689°
Mean anomaly
85.051°
Eccentric anomaly
85.14394°
Mean motion
3.9577 °/min
Orbital period
90.96 mins
BSTAR
0.026283
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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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