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)
NOAA 16 DEB details
Identifier | |
Orbit | Decayed |
Last TLE update | 3 months ago |
Origin | |
Manufacturer | Unknown |
Mission | Decayed spacecraft |
Bus & Motor | Unknown |
Mass | Unknown |
Launch date (UTC) | |
Launch vehicle | Unknown |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Unknown |
Radar Cross Section | Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 3 months 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
Definitive object data (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 | Object was in daylight at TLE epoch |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
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 |
BSTAR | 0.026432 |
Orbital period | 94.56 mins |
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Other satellites on launch #55 in the year 2000 (2000-09-21 UTC)
NOAA 16 DEB Visibility forecast
Observer location: undefined°, undefined
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