NOAA 17 DEB, 49481 (Decayed)
Orbit data source: Space-Track
NOAA 17 DEB, 49481 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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49481 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 3 months ago
TLE from 3 months ago
0 NOAA 17 DEB
1 49481U 02032DK 26079.48456561 .00627126 00000-0 13103-1 0 9999
2 49481 98.6638 94.3828 0013949 133.3302 226.9107 15.43008885252168Epoch: 2026-03-20T11:37Z
TLE epoch observation values (Epoch: 2026-03-20T11:37:46.468Z)
Latitude
-0.00003°
Longitude
101.92022°
Altitude
446.82 km
Speed
7.64 km/s
True Right ascension
06h 17m 31s
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
21:35:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
443.732 km
Perigee altitude
424.726 km
Semi-major axis
6,812.366 km
Eccentricity
0.00139
Inclination
98.6638°
RAAN
94.3828°
Arg. of periapsis
133.3302°
True anomaly
226.79411°
Mean anomaly
226.9107°
Eccentric anomaly
226.85239°
Mean motion
3.86008 °/min
Orbital period
93.26 mins
BSTAR
0.013103
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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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