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IUS R/B(2) (16119)
COSPAR: 1985-092E | Alt Name: IUS-12 SRM-2
Image
Additional Sources
Launch Details
Launch Date
October 3, 1985
Launch Site
Launch Pad
LC39A
Launch Vehicle
Space Shuttle
Orbital Elements
NORAD ID
16119
International Designator
1985-092E
Epoch
Sat, 04 Jul 2026 03:15:54 GMT
Apogee
Calculating...
Perigee
Calculating...
Inclination
10.02°
Right Ascension
314.59°
Eccentricity
Calculating...
Argument of Perigee
181.86°
Period
1424.58 min
Mean Motion
1.01 rev/day
Latitude
Calculating...
Longitude
Calculating...
Altitude
Calculating...
Velocity
Calculating...
Polar Plot
3D Visualization
Basic Satellite Info
Name
IUS R/B(2)
Alternative Name
IUS-12 SRM-2
Type
Rocket Body
Status
Space Junk
Owner
AFSD
Country
United States
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 16119U 85092E 26185.13604630 .00000007 00000+0 00000+0 0 9992
2 16119 10.0179 314.5912 0056894 181.8591 178.2225 01.01082220 26223
Source: Celestrak
Summary
A rocket body, also commonly referred to as an upper stage or spent rocket stage, is the structural shell left behind after a rocket has delivered its payload to orbit. These large and often heavy pieces of space hardware can remain in orbit for years, posing significant collision hazards as part of the growing space debris problem. If left uncontrolled, rocket bodies have the potential to reenter Earth's atmosphere unpredictably, which can lead to falling debris in populated areas. Additionally, they risk colliding with operational satellites or the International Space Station, creating more debris and putting human life at risk.
Physical Characteristics
Length
2.1
Diameter
1.6
Span
2.1
Dry Mass
1100
Launch Mass
3800
Shape
Sphere + Cone
Radar Cross Section
Unknown
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
Orbus 6E
Purpose
Unknown
Mission
Unknown
Manufacturer
CSD
Life Expectancy
Unknown
Bus
Orbus 6
Configuration
Unknown
Motor
Unknown
Equipment
Unknown
Power System
Unknown
ADCS
Unknown
Transmitter Frequency
Unknown
Map
Next Pass
Azimuth Elevation Time (Local)
Start Azimuth
Max Elevation
Stop Azimuth
Time Until
Pass Duration
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