NOAA 16 DEB, 42412 (Decayed)
Orbit data source: Space-Track
NOAA 16 DEB, 42412 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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42412 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: 1 month ago
TLE from 1 month ago
0 NOAA 16 DEB
1 42412U 00055TG 25298.38191848 .04601745 00000-0 33125-1 0 9993
2 42412 98.7569 86.5309 0031048 313.7224 46.1462 15.68922002500090Epoch: 2025-10-25T09:09Z
TLE epoch observation values (Epoch: 2025-10-25T09:09:57.756Z)
Latitude
-0.00008°
Longitude
-84.97301°
Altitude
350.628 km
Speed
7.707 km/s
True Right ascension
05h 46m 07s
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
15:04:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
379.865 km
Perigee altitude
338.031 km
Semi-major axis
6,737.085 km
Eccentricity
0.0031
Inclination
98.7569°
RAAN
86.5309°
Arg. of periapsis
313.7224°
True anomaly
46.40345°
Mean anomaly
46.1462°
Eccentric anomaly
46.27476°
Mean motion
3.92496 °/min
Orbital period
91.72 mins
BSTAR
0.033125
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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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