IUS R/B(2), 26883
Orbit data source: Space-Track
IUS R/B(2), 26883 is space debris in GEO originally from a launch on Mon, 06 Aug 2001 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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26883 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 IUS R/B(2)
1 26883U 01033D 26275.84152789 .00000063 00000-0 00000-0 0 9999
2 26883 13.0277 15.9445 0006356 10.3870 349.6353 0.99885986 26863Epoch: 2026-10-02T20:11Z
TLE epoch observation values (Epoch: 2026-10-02T20:11:48.009Z)
Latitude
0.00001°
Longitude
61.42235°
Altitude
35,868.108 km
Speed
3.073 km/s
True Right ascension
01h 03m 43s
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
01:33:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,922.954 km
Perigee altitude
35,869.215 km
Semi-major axis
42,274.222 km
Eccentricity
0.00064
Inclination
13.0277°
RAAN
15.9445°
Arg. of periapsis
10.387°
True anomaly
349.62219°
Mean anomaly
349.6353°
Eccentric anomaly
349.62874°
Mean motion
0.24971 °/min
Orbital period
1,441.69 mins
BSTAR
0
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Other satellites on launch #33 in the year 2001 (2001-08-06 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 R/B(2) 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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| IUS R/B(2) is likely not visible in the next few days. |
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26883 neighbors
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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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