NOAA 16 DEB, 41076 (Decayed)
Orbit data source: Space-Track
NOAA 16 DEB, 41076 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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41076 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 week ago
TLE from 1 week ago
0 NOAA 16 DEB
1 41076U 00055AK 26119.18648391 .06540140 35038-5 39935-2 0 9992
2 41076 99.1417 357.5581 0014003 243.4698 116.5149 16.17907940558659Epoch: 2026-04-29T04:28Z
TLE epoch observation values (Epoch: 2026-04-29T04:28:32.209Z)
Latitude
-0.00002°
Longitude
73.27284°
Altitude
232.542 km
Speed
7.765 km/s
True Right ascension
23h 50m 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
05:42:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
231.403 km
Perigee altitude
212.919 km
Semi-major axis
6,600.298 km
Eccentricity
0.0014
Inclination
99.1417°
RAAN
357.5581°
Arg. of periapsis
243.4698°
True anomaly
116.65837°
Mean anomaly
116.5149°
Eccentric anomaly
116.58665°
Mean motion
4.0476 °/min
Orbital period
88.94 mins
BSTAR
0.0039935
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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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