NOAA 16 DEB, 42338 (Decayed)
Orbit data source: Space-Track
NOAA 16 DEB, 42338 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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42338 intel report (Beta)
NOAA 16 DEB details
Identifier | |
Orbit | Decayed |
Last TLE update | 2 weeks 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 2 weeks ago
0 NOAA 16 DEB
1 42338U 00055QE 24325.37762461 .03166497 00000-0 35199-1 0 9996
2 42338 98.6743 109.0176 0029406 302.4142 57.4266 15.58647458456794
Epoch: 2024-11-20T09:03Z
Definitive object data (Epoch: 2024-11-20T09:03:46.766Z)
Latitude | -0.00001° |
Longitude | -86.80184° |
Altitude | 383.995 km |
Speed | 7.686 km/s |
True Right ascension | 07h 16m 04s |
True Declination | 0° 00' 00" |
Sunlit | Object was in full shadow 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 | 408.443 km |
Perigee altitude | 368.647 km |
Semi-major axis | 6,766.682 km |
Eccentricity | 0.0029406 |
Inclination | 98.6743° |
RAAN | 109.0176° |
Arg. of periapsis | 302.4142° |
True anomaly | 57.71113° |
Mean anomaly | 57.4266° |
Eccentric anomaly | 57.56881° |
Mean motion | 3.89924 °/min |
BSTAR | 0.035199 |
Orbital period | 92.33 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
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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