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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Identifier
16118, 1985-092D
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
UTC CSD
Mission
Spacecraft
Bus & Motor
ORBUS 21, Unknown motor
Mass
~1,164 kg wet, ~1,164 kg dry
Launch date (UTC)
1985-10-03 (40 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, Unknown HBR
Radar Cross Section
7.708 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago
0 IUS R/B(1)
1 16118U 85092D   25259.13540348  .00000240  00000-0  84155-3 0  9994
2 16118  25.3159 257.3174 7189021  17.2864 358.0628  2.29064697 54533
Epoch: 2025-09-16T03:14Z
TLE epoch observation values (Epoch: 2025-09-16T03:14:58.86Z)
Latitude
0.0004°
Longitude
-146.79466°
Altitude
600.207 km
Speed
9.891 km/s
True Right ascension
17h 09m 07s
True Declination
0° 00' 01"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
19:08:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,413.022 km
Perigee altitude
456.113 km
Semi-major axis
24,312.705 km
Eccentricity
0.7189
Inclination
25.3159°
RAAN
257.3174°
Arg. of periapsis
17.2864°
True anomaly
343.1634°
Mean anomaly
358.0628°
Eccentric anomaly
353.15015°
Mean motion
0.57252 °/min
Orbital period
628.8 mins
BSTAR
0.00084155
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Other satellites on launch #92 in the year 1985 (1985-10-03 UTC)

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