NOAA 16 DEB, 41528 (Decayed)
Orbit data source: Space-Track
NOAA 16 DEB, 41528 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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41528 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: 2 months ago
TLE from 2 months ago
0 NOAA 16 DEB
1 41528U 00055NC 25352.80470419 .00577957 00000-0 15838-1 0 9996
2 41528 98.7238 121.3801 0027592 294.1532 65.6822 15.34608720507339Epoch: 2025-12-18T19:18Z
TLE epoch observation values (Epoch: 2025-12-18T19:18:46.442Z)
Latitude
-0.00004°
Longitude
104.03165°
Altitude
457.421 km
Speed
7.642 km/s
True Right ascension
08h 05m 31s
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
12:27:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
477.956 km
Perigee altitude
440.226 km
Semi-major axis
6,837.228 km
Eccentricity
0.00276
Inclination
98.7238°
RAAN
121.3801°
Arg. of periapsis
294.1532°
True anomaly
65.97074°
Mean anomaly
65.6822°
Eccentric anomaly
65.82643°
Mean motion
3.83904 °/min
Orbital period
93.77 mins
BSTAR
0.015838
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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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