IUS DEB, 43361
Orbit data source: Space-Track
IUS DEB, 43361 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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43361 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
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 IUS DEB
1 43361U 99040J 25216.30800218 .00000347 00000-0 75119-2 0 9996
2 43361 27.8445 238.2199 3364172 206.4873 131.5407 7.21211150260413Epoch: 2025-08-04T07:23Z
TLE epoch observation values (Epoch: 2025-08-04T07:23:31.388Z)
Latitude
-0.00001°
Longitude
174.22177°
Altitude
7,980.621 km
Speed
4.506 km/s
True Right ascension
15h 52m 52s
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
16:53:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
8,748.982 km
Perigee altitude
1,133.062 km
Semi-major axis
11,319.159 km
Eccentricity
0.33642
Inclination
27.8445°
RAAN
238.2199°
Arg. of periapsis
206.4873°
True anomaly
153.54922°
Mean anomaly
131.5407°
Eccentric anomaly
143.11101°
Mean motion
1.80228 °/min
Orbital period
199.75 mins
BSTAR
0.0075119
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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. |
|---|---|---|---|---|---|---|---|
| 97 mins | 2025-09-14 01:04:38.152Z | 255.128° W | 2025-09-14 01:38:38.152Z | 178.662° S | 42.843° | 2025-09-14 02:41:38.152Z | 110.881° ESE |
| 96 mins | 2025-09-14 04:48:38.152Z | 275.364° WNW | 2025-09-14 05:39:38.152Z | 218.082° SW | 36.618° | 2025-09-14 06:24:38.152Z | 153.087° SSE |
| 50 mins | 2025-09-14 20:49:38.152Z | 194.802° SSW | 2025-09-14 21:02:38.152Z | 137.448° SSE | 31.541° | 2025-09-14 21:39:38.152Z | 82.676° 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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