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
Country
USRelated business
Manufacturer
Unknown
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 9 months ago
TLE from 9 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 15.27804096451482Epoch: 2024-12-21T10:47Z
TLE epoch observation values (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
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
15:48:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
492.701 km
Perigee altitude
466.102 km
Semi-major axis
6,857.539 km
Eccentricity
0.00194
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
Orbital period
94.19 mins
BSTAR
0.028765
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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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