NOAA 17 DEB, 48757 (Decayed)
Orbit data source: Space-Track
NOAA 17 DEB, 48757 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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48757 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: 6 months ago
TLE from 6 months ago
0 NOAA 17 DEB
1 48757U 02032CS 25155.90231784 .01290146 00000-0 17769-1 0 9994
2 48757 98.5955 146.8951 0018975 137.1091 223.1643 15.54359248220214Epoch: 2025-06-04T21:39Z
TLE epoch observation values (Epoch: 2025-06-04T21:39:20.261Z)
Latitude
-0.00001°
Longitude
-71.51795°
Altitude
416.516 km
Speed
7.656 km/s
True Right ascension
09h 47m 34s
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
08:21:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
413.855 km
Perigee altitude
388.128 km
Semi-major axis
6,779.129 km
Eccentricity
0.0019
Inclination
98.5955°
RAAN
146.8951°
Arg. of periapsis
137.1091°
True anomaly
223.01581°
Mean anomaly
223.1643°
Eccentric anomaly
223.09003°
Mean motion
3.8885 °/min
Orbital period
92.58 mins
BSTAR
0.017769
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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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