NOAA 16 DEB, 41345 (Decayed)
Orbit data source: Space-Track
NOAA 16 DEB, 41345 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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41345 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
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 NOAA 16 DEB
1 41345U 00055HN 24134.12307769 .05907931 00000-0 33553-1 0 9990
2 41345 98.7864 357.4052 0014302 247.8034 112.1709 15.74604459436958Epoch: 2024-05-13T02:57Z
TLE epoch observation values (Epoch: 2024-05-13T02:57:13.912Z)
Latitude
-0.00003°
Longitude
81.7322°
Altitude
352.518 km
Speed
7.695 km/s
True Right ascension
23h 49m 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
21:23:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
352.329 km
Perigee altitude
333.104 km
Semi-major axis
6,720.853 km
Eccentricity
0.00143
Inclination
98.7864°
RAAN
357.4052°
Arg. of periapsis
247.8034°
True anomaly
112.32257°
Mean anomaly
112.1709°
Eccentric anomaly
112.24674°
Mean motion
3.93919 °/min
Orbital period
91.39 mins
BSTAR
0.033553
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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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