NOAA 16 DEB, 42346 (Decayed)
Orbit data source: Space-Track
NOAA 16 DEB, 42346 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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42346 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 NOAA 16 DEB
1 42346U 00055QN 24266.00932353 .00653240 00000-0 26432-1 0 9992
2 42346 99.0137 179.7295 0025800 85.0696 275.3479 15.21920337452875
Epoch: 2024-09-22T00:13Z
TLE epoch observation values (Epoch: 2024-09-22T00:13:25.552Z)
Latitude
-0.00013°
Longitude
175.01468°
Altitude
501.482 km
Speed
7.615 km/s
True Right ascension
11h 58m 55s
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
05:28:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
514.826 km
Perigee altitude
479.35 km
Semi-major axis
6,875.225 km
Eccentricity
0.00258
Inclination
99.0137°
RAAN
179.7295°
Arg. of periapsis
85.0696°
True anomaly
275.05345°
Mean anomaly
275.3479°
Eccentric anomaly
275.20069°
Mean motion
3.80726 °/min
Orbital period
94.56 mins
BSTAR
0.026432
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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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