NOAA 16 DEB, 41127
Orbit data source: Space-Track
NOAA 16 DEB, 41127 is 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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41127 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 5 days ago
TLE from 5 days ago
0 NOAA 16 DEB
1 41127U 00055BJ 25336.66811027 .05374670 00000-0 21050-1 0 9996
2 41127 98.8145 240.5880 0014223 113.5217 246.7543 15.82747749527011Epoch: 2025-12-02T16:02Z
TLE epoch observation values (Epoch: 2025-12-02T16:02:04.727Z)
Latitude
-0.00007°
Longitude
-71.68164°
Altitude
329.578 km
Speed
7.709 km/s
True Right ascension
16h 02m 21s
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
05:22:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
329.151 km
Perigee altitude
310.098 km
Semi-major axis
6,697.761 km
Eccentricity
0.00142
Inclination
98.8145°
RAAN
240.588°
Arg. of periapsis
113.5217°
True anomaly
246.60465°
Mean anomaly
246.7543°
Eccentric anomaly
246.67947°
Mean motion
3.95958 °/min
Orbital period
90.92 mins
BSTAR
0.02105
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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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| NOAA 16 DEB is likely not visible in the next few days. |
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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