NOAA 17 DEB, 49484 (Decayed)
Orbit data source: Space-Track
NOAA 17 DEB, 49484 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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49484 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: 8 months ago
TLE from 8 months ago
0 NOAA 17 DEB
1 49484U 02032DN 25098.40641204 .00817052 00000-0 30552-1 0 9990
2 49484 98.6543 86.3631 0023891 121.3823 238.9752 15.24481952199383Epoch: 2025-04-08T09:45Z
TLE epoch observation values (Epoch: 2025-04-08T09:45:14.000Z)
Latitude
-0.00004°
Longitude
103.14683°
Altitude
503.89 km
Speed
7.608 km/s
True Right ascension
05h 45m 27s
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
08:24:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.766 km
Perigee altitude
472.952 km
Semi-major axis
6,867.496 km
Eccentricity
0.00239
Inclination
98.6543°
RAAN
86.3631°
Arg. of periapsis
121.3823°
True anomaly
238.74095°
Mean anomaly
238.9752°
Eccentric anomaly
238.85804°
Mean motion
3.81369 °/min
Orbital period
94.4 mins
BSTAR
0.030552
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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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