NOAA 17 DEB, 49482
Orbit data source: Space-Track
NOAA 17 DEB, 49482 is space debris in SSO originally from a launch on Mon, 24 Jun 2002 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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49482 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 NOAA 17 DEB
1 49482U 02032DL 25316.84610264 .00823029 00000-0 23686-1 0 9992
2 49482 98.7018 353.8429 0008041 203.5017 156.5855 15.33245165233320Epoch: 2025-11-12T20:18Z
TLE epoch observation values (Epoch: 2025-11-12T20:18:23.268Z)
Latitude
0.00001°
Longitude
-2.9665°
Altitude
474.258 km
Speed
7.626 km/s
True Right ascension
23h 35m 22s
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
15:09:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
468.648 km
Perigee altitude
457.645 km
Semi-major axis
6,841.284 km
Eccentricity
0.0008
Inclination
98.7018°
RAAN
353.8429°
Arg. of periapsis
203.5017°
True anomaly
156.62208°
Mean anomaly
156.5855°
Eccentric anomaly
156.60379°
Mean motion
3.83563 °/min
Orbital period
93.86 mins
BSTAR
0.023686
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Other satellites on launch #32 in the year 2002 (2002-06-24 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 17 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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| NOAA 17 DEB is likely not visible in the next few days. |
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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