NOAA 16 DEB, 41664 (Decayed)
Orbit data source: Space-Track
NOAA 16 DEB, 41664 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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41664 intel report (Beta)
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Edit Public Description
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 41664U 00055PD 24356.44965467 .00850626 00000-0 28765-1 0 9992
2 41664 98.8529 168.0264 0019394 302.0488 57.8862 15.27804096451482
Epoch: 2024-12-21T10:47Z
Definitive object data (Epoch: 2024-12-21T10:47:30.163Z)
Latitude | -0.00011° |
Longitude | -84.34991° |
Altitude | 478.377 km |
Speed | 7.63 km/s |
True Right ascension | 11h 12m 06s |
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 | 492.701 km |
Perigee altitude | 466.102 km |
Semi-major axis | 6,857.539 km |
Eccentricity | 0.0019394 |
Inclination | 98.8529° |
RAAN | 168.0264° |
Arg. of periapsis | 302.0488° |
True anomaly | 58.07468° |
Mean anomaly | 57.8862° |
Eccentric anomaly | 57.98041° |
Mean motion | 3.822 °/min |
BSTAR | 0.028765 |
Orbital period | 94.19 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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