NOAA 17 DEB, 48176 (Decayed)
Orbit data source: Space-Track
NOAA 17 DEB, 48176 was 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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48176 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 shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 3 months ago
TLE from 3 months ago
0 NOAA 17 DEB
1 48176U 02032R 25271.03800245 .00634177 00000-0 14853-1 0 9992
2 48176 98.6589 295.9280 0004497 149.9498 210.2003 15.39942196240379Epoch: 2025-09-28T00:54Z
TLE epoch observation values (Epoch: 2025-09-28T00:54:43.411Z)
Latitude
-0.00002°
Longitude
-84.81469°
Altitude
452.012 km
Speed
7.64 km/s
True Right ascension
19h 43m 42s
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
13:19:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
446.346 km
Perigee altitude
440.21 km
Semi-major axis
6,821.415 km
Eccentricity
0.00045
Inclination
98.6589°
RAAN
295.928°
Arg. of periapsis
149.9498°
True anomaly
210.17439°
Mean anomaly
210.2003°
Eccentric anomaly
210.18734°
Mean motion
3.8524 °/min
Orbital period
93.45 mins
BSTAR
0.014853
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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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| 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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