NOAA 16 DEB, 42336 (Decayed)
Orbit data source: Space-Track
NOAA 16 DEB, 42336 was space debris in LEO 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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42336 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 42336U 00055QC 24254.49431937 .20037488 00000-0 84361-1 0 9990
2 42336 98.8004 80.8964 0018276 299.5154 60.4285 15.79457418441019
Epoch: 2024-09-10T11:51Z
Definitive object data (Epoch: 2024-09-10T11:51:49.193Z)
Latitude | -0.00012° |
Longitude | -87.06719° |
Altitude | 329.066 km |
Speed | 7.714 km/s |
True Right ascension | 05h 23m 35s |
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 | 341.189 km |
Perigee altitude | 316.673 km |
Semi-major axis | 6,707.068 km |
Eccentricity | 0.0018276 |
Inclination | 98.8004° |
RAAN | 80.8964° |
Arg. of periapsis | 299.5154° |
True anomaly | 60.61085° |
Mean anomaly | 60.4285° |
Eccentric anomaly | 60.51966° |
Mean motion | 3.95134 °/min |
BSTAR | 0.084361 |
Orbital period | 91.11 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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