IUS R/B(1), 16118
Orbit data source: Space-Track
IUS R/B(1), 16118 is space debris in HEO originally from a launch on Thu, 03 Oct 1985 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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16118 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
UTC CSD
Mission
Spacecraft
Bus & Motor
ORBUS 21, Unknown motor
Mass
~1,164 kg wet, ~1,164 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 IUS R/B(1)
1 16118U 85092D 25348.60749385 .00000381 00000-0 13200-2 0 9995
2 16118 24.9744 224.3079 7199300 72.8047 349.3747 2.29131665 56589Epoch: 2025-12-14T14:34Z
TLE epoch observation values (Epoch: 2025-12-14T14:34:47.468Z)
Latitude
0.00003°
Longitude
-77.78574°
Altitude
3,250.954 km
Speed
8.148 km/s
True Right ascension
14h 57m 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
13:22:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,429.963 km
Perigee altitude
429.811 km
Semi-major axis
24,308.024 km
Eccentricity
0.71993
Inclination
24.9744°
RAAN
224.3079°
Arg. of periapsis
72.8047°
True anomaly
287.03766°
Mean anomaly
349.3747°
Eccentric anomaly
326.77056°
Mean motion
0.57269 °/min
Orbital period
628.61 mins
BSTAR
0.00132
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Other satellites on launch #92 in the year 1985 (1985-10-03 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(1) 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(1) is likely not visible in the next few days. |
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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