NOAA 16 DEB, 42369 (Decayed)
Orbit data source: Space-Track
NOAA 16 DEB, 42369 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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42369 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
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 42369U 00055RM 25221.89726395 .05077252 00000-0 37681-1 0 9999
2 42369 98.7324 355.7779 0036427 307.1884 52.6049 15.67570498493380Epoch: 2025-08-09T21:32Z
TLE epoch observation values (Epoch: 2025-08-09T21:32:03.605Z)
Latitude
0.00001°
Longitude
74.1365°
Altitude
354.103 km
Speed
7.705 km/s
True Right ascension
23h 43m 06s
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
23:17:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
387.377 km
Perigee altitude
338.267 km
Semi-major axis
6,740.959 km
Eccentricity
0.00364
Inclination
98.7324°
RAAN
355.7779°
Arg. of periapsis
307.1884°
True anomaly
52.93745°
Mean anomaly
52.6049°
Eccentric anomaly
52.77108°
Mean motion
3.92158 °/min
Orbital period
91.8 mins
BSTAR
0.037681
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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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