NOAA 16 DEB, 41256
Orbit data source: Space-Track
NOAA 16 DEB, 41256 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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41256 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
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: 6 hours ago
TLE from 6 hours ago
0 NOAA 16 DEB
1 41256U 00055FG 25341.94092966 .00016697 00000-0 40798-2 0 9997
2 41256 99.0917 228.5822 0017163 5.1692 354.9675 14.52555514516362Epoch: 2025-12-07T22:34Z
TLE epoch observation values (Epoch: 2025-12-07T22:34:56.322Z)
Latitude
-0.00006°
Longitude
172.90044°
Altitude
708.127 km
Speed
7.508 km/s
True Right ascension
15h 14m 19s
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
02:48:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
726.621 km
Perigee altitude
702.275 km
Semi-major axis
7,092.585 km
Eccentricity
0.00172
Inclination
99.0917°
RAAN
228.5822°
Arg. of periapsis
5.1692°
True anomaly
354.95021°
Mean anomaly
354.9675°
Eccentric anomaly
354.95886°
Mean motion
3.63359 °/min
Orbital period
99.08 mins
BSTAR
0.0040798
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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 forecast
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-12-08 05:45:15.983Z | 8.55° NNE | 2025-12-08 05:50:15.983Z | 255.134° W | 42.289° | 2025-12-08 05:54:15.983Z | 205.149° SW |
| 7 mins | 2025-12-08 16:54:15.983Z | 189.413° SSW | 2025-12-08 16:57:15.983Z | 277.894° WNW | 38.964° | 2025-12-08 17:01:15.983Z | 336.054° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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