IRIDIUM 47 DEB, 40249
Orbit data source: Space-Track
IRIDIUM 47 DEB, 40249 is space debris in LEO originally from a launch on Sat, 20 Dec 1997 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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40249 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
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 hours ago
TLE from 6 hours ago
0 IRIDIUM 47 DEB
1 40249U 97082J 25343.58360277 .00002217 00000-0 66900-3 0 9996
2 40249 86.3907 32.1008 0002399 91.7974 268.3501 14.42094804587593Epoch: 2025-12-09T14:00Z
TLE epoch observation values (Epoch: 2025-12-09T14:00:23.279Z)
Latitude
-0.00001°
Longitude
103.43761°
Altitude
754.697 km
Speed
7.477 km/s
True Right ascension
02h 08m 24s
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
18:44:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
750.249 km
Perigee altitude
746.829 km
Semi-major axis
7,126.676 km
Eccentricity
0.00024
Inclination
86.3907°
RAAN
32.1008°
Arg. of periapsis
91.7974°
True anomaly
268.32262°
Mean anomaly
268.3501°
Eccentric anomaly
268.33636°
Mean motion
3.60755 °/min
Orbital period
99.79 mins
BSTAR
0.000669
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Other satellites on launch #82 in the year 1997 (1997-12-20 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.IRIDIUM 47 DEB Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-12-10 03:26:58.633Z | 152.07° SSE | 2025-12-10 03:30:58.633Z | 81.699° E | 33.896° | 2025-12-10 03:34:58.633Z | 19.354° NNE |
| 5 mins | 2025-12-10 05:08:58.633Z | 250.69° W | 2025-12-10 05:10:58.633Z | 279.528° WNW | 18.744° | 2025-12-10 05:13:58.633Z | 321.588° NNW |
| 9 mins | 2025-12-10 15:33:58.633Z | 356.795° N | 2025-12-10 15:37:58.633Z | 262.875° W | 44.969° | 2025-12-10 15:42:58.633Z | 180.146° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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