NOAA 17 DEB, 48612 (Decayed)
Orbit data source: Space-Track
NOAA 17 DEB, 48612 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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48612 intel report (Beta)
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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
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 NOAA 17 DEB
1 48612U 02032AD 25053.54763246 .04211581 00000-0 21162-1 0 9995
2 48612 98.6529 83.9851 0009657 194.5650 165.5336 15.78152307206638Epoch: 2025-02-22T13:08Z
TLE epoch observation values (Epoch: 2025-02-22T13:08:35.444Z)
Latitude
-0°
Longitude
94.14441°
Altitude
345.085 km
Speed
7.698 km/s
True Right ascension
05h 35m 56s
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
21:36:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
339.104 km
Perigee altitude
326.143 km
Semi-major axis
6,710.761 km
Eccentricity
0.00097
Inclination
98.6529°
RAAN
83.9851°
Arg. of periapsis
194.565°
True anomaly
165.56121°
Mean anomaly
165.5336°
Eccentric anomaly
165.54741°
Mean motion
3.94808 °/min
Orbital period
91.18 mins
BSTAR
0.021162
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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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