IUS DEB, 43362
Orbit data source: Space-Track
IUS DEB, 43362 is space debris originally from a launch on Fri, 23 Jul 1999 UTC launched from the Air Force Eastern Test Range (AFETR). 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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43362 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Boeing/Kent
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: 3 weeks ago
TLE from 3 weeks ago
0 IUS DEB
1 43362U 99040K 25278.48370013 -.00001219 00000-0 -10221-1 0 9992
2 43362 28.0688 224.9823 3683344 197.0371 146.3312 7.09380226250139Epoch: 2025-10-05T11:36Z
TLE epoch observation values (Epoch: 2025-10-05T11:36:31.691Z)
Latitude
-0.00001°
Longitude
36.44959°
Altitude
8,886.482 km
Speed
4.171 km/s
True Right ascension
14h 59m 55s
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
13:19:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
9,282.031 km
Perigee altitude
851.082 km
Semi-major axis
11,444.694 km
Eccentricity
0.36833
Inclination
28.0688°
RAAN
224.9823°
Arg. of periapsis
197.0371°
True anomaly
162.99888°
Mean anomaly
146.3312°
Eccentric anomaly
155.1875°
Mean motion
1.77271 °/min
Orbital period
203.08 mins
BSTAR
-0.010221
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Other satellites on launch #40 in the year 1999 (1999-07-23 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.IUS 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-10-29 17:46:15.038Z | 86.493° E | 2025-10-29 17:46:15.038Z | 86.493° E | 16.437° | 2025-10-29 17:58:15.038Z | 80.142° E |
| 109 mins | 2025-10-29 20:16:15.038Z | 234.034° WSW | 2025-10-29 21:05:15.038Z | 161.5° S | 42.417° | 2025-10-29 22:05:15.038Z | 94.38° ESE |
| 99 mins | 2025-10-30 00:09:15.038Z | 268.886° W | 2025-10-30 01:16:15.038Z | 205.931° SW | 41.369° | 2025-10-30 01:48:15.038Z | 131.32° SE |
| 43 mins | 2025-10-30 04:34:15.038Z | 275.599° WNW | 2025-10-30 05:02:15.038Z | 240.237° WSW | 19.925° | 2025-10-30 05:17:15.038Z | 197.977° SSW |
| 69 mins | 2025-10-30 16:23:15.038Z | 171.607° S | 2025-10-30 16:45:15.038Z | 124.428° SE | 25.135° | 2025-10-30 17:32:15.038Z | 80.588° E |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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