IUS R/B(2), 22316
Orbit data source: Space-Track
IUS R/B(2), 22316 is space debris in GEO originally from a launch on Wed, 13 Jan 1993 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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22316 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 IUS R/B(2)
1 22316U 93003D 25259.84439706 -.00000376 00000-0 00000-0 0 9990
2 22316 12.0204 346.0432 0068627 120.2555 307.8925 1.00112577124450
Epoch: 2025-09-16T20:15Z
TLE epoch observation values (Epoch: 2025-09-16T20:15:55.905Z)
Latitude
11.09416°
Longitude
113.09927°
Altitude
35,654.875 km
Speed
3.086 km/s
True Right ascension
03h 32m 26s
True Declination
11° 04' 59"
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
17:34:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,121.965 km
Perigee altitude
35,542.61 km
Semi-major axis
42,210.424 km
Eccentricity
0.00686
Inclination
12.0204°
RAAN
346.0432°
Arg. of periapsis
120.2555°
True anomaly
307.26862°
Mean anomaly
307.8925°
Eccentric anomaly
307.58089°
Mean motion
0.25027 °/min
Orbital period
1,438.43 mins
BSTAR
0
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Other satellites on launch #3 in the year 1993 (1993-01-13 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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22316 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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