NOAA 16 DEB, 41250 (Decayed)
Orbit data source: Space-Track
NOAA 16 DEB, 41250 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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41250 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 41250U 00055FA 26045.56296821 .01744955 00000-0 21693-1 0 9995
2 41250 98.9701 262.0562 0010059 16.5566 343.6010 15.56862566527758Epoch: 2026-02-14T13:30Z
TLE epoch observation values (Epoch: 2026-02-14T13:30:40.453Z)
Latitude
-0.00008°
Longitude
-85.19657°
Altitude
393.295 km
Speed
7.678 km/s
True Right ascension
17h 28m 13s
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
16:21:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
400.547 km
Perigee altitude
386.924 km
Semi-major axis
6,771.873 km
Eccentricity
0.00101
Inclination
98.9701°
RAAN
262.0562°
Arg. of periapsis
16.5566°
True anomaly
343.56842°
Mean anomaly
343.601°
Eccentric anomaly
343.58471°
Mean motion
3.89475 °/min
Orbital period
92.43 mins
BSTAR
0.021693
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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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