IUS DEB, 26076
Orbit data source: Space-Track
IUS DEB, 26076 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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26076 intel report (Beta)
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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
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 weeks ago
TLE from 2 weeks ago
0 IUS DEB
1 26076U 99040E 26249.14763407 .00001186 00000-0 37046-3 0 9997
2 26076 28.4092 71.2039 4312651 193.7234 149.3608 6.70735093533519Epoch: 2026-09-06T03:32Z
TLE epoch observation values (Epoch: 2026-09-06T03:32:35.583Z)
Latitude
-0.00002°
Longitude
32.80867°
Altitude
10,260.058 km
Speed
3.79 km/s
True Right ascension
04h 44m 48s
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
16:02:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
10,625.564 km
Perigee altitude
378.541 km
Semi-major axis
11,880.19 km
Eccentricity
0.43127
Inclination
28.4092°
RAAN
71.2039°
Arg. of periapsis
193.7234°
True anomaly
166.3125°
Mean anomaly
149.3608°
Eccentric anomaly
158.44071°
Mean motion
1.67613 °/min
Orbital period
214.78 mins
BSTAR
0.00037046
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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. |
|---|---|---|---|---|---|---|---|
| 115 mins | 2026-09-23 09:43:36.733Z | 191.391° SSW | 2026-09-23 10:29:36.733Z | 130.048° SE | 41.651° | 2026-09-23 11:38:36.733Z | 80.528° E |
| 126 mins | 2026-09-23 13:37:36.733Z | 242.348° WSW | 2026-09-23 14:58:36.733Z | 176.061° S | 70.317° | 2026-09-23 15:43:36.733Z | 101.21° ESE |
| 82 mins | 2026-09-23 18:08:36.733Z | 276.5° WNW | 2026-09-23 19:13:36.733Z | 218.947° SW | 48.369° | 2026-09-23 19:30:36.733Z | 150.218° SSE |
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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