NOAA 16 DEB, 42361 (Decayed)
Orbit data source: Space-Track
NOAA 16 DEB, 42361 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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42361 intel report (Beta)
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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 42361U 00055RD 26097.87289606 .01780316 00000-0 22842-1 0 9991
2 42361 98.8876 244.8667 0031284 304.7816 55.0490 15.55556457528217Epoch: 2026-04-07T20:56Z
TLE epoch observation values (Epoch: 2026-04-07T20:56:58.219Z)
Latitude
-0.00004°
Longitude
94.48075°
Altitude
391.52 km
Speed
7.682 km/s
True Right ascension
16h 19m 28s
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
03:08:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
418.722 km
Perigee altitude
376.328 km
Semi-major axis
6,775.662 km
Eccentricity
0.00313
Inclination
98.8876°
RAAN
244.8667°
Arg. of periapsis
304.7816°
True anomaly
55.34349°
Mean anomaly
55.049°
Eccentric anomaly
55.19618°
Mean motion
3.89149 °/min
Orbital period
92.51 mins
BSTAR
0.022842
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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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