IUS R/B(2), 16119
Orbit data source: Space-Track
IUS R/B(2), 16119 is space debris in GEO 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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16119 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
UTC CSD
Mission
Orbus 6E) (Atlantis (OV-104))"
Bus & Motor
ORBUS 6, Unknown motor
Mass
~1,100 kg wet, ~1,100 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, Unknown HBR
Radar Cross Section
8.086 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 IUS R/B(2)
1 16119U 85092E 25259.30665676 .00000030 00000-0 00000-0 0 9997
2 16119 10.5448 316.8074 0058649 175.8261 184.2222 1.01086454 23288Epoch: 2025-09-16T07:21Z
TLE epoch observation values (Epoch: 2025-09-16T07:21:35.144Z)
Latitude
0.00001°
Longitude
-149.07296°
Altitude
35,805.059 km
Speed
3.065 km/s
True Right ascension
21h 07m 17s
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
16:58:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,806.74 km
Perigee altitude
35,314.805 km
Semi-major axis
41,938.909 km
Eccentricity
0.00586
Inclination
10.5448°
RAAN
316.8074°
Arg. of periapsis
175.8261°
True anomaly
184.17308°
Mean anomaly
184.2222°
Eccentric anomaly
184.1976°
Mean motion
0.25271 °/min
Orbital period
1,424.57 mins
BSTAR
0
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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(2) 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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2025-09-17 00:13:45.494Z | 226.867° WSW | 2025-09-17 13:36:45.494Z | 242.129° WSW | 30.698° | 2025-09-18 00:13:45.494Z | 224.002° SW |
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16119 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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