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OV1-14 R/B (03177)
COSPAR: 1968-026C | Alt Name: OV1-14P
Image
Additional Sources
Launch Details
Launch Date
April 6, 1968
Launch Site
AFWTR
Launch Pad
ABRESA2
Launch Vehicle
Atlas F
Orbital Elements
NORAD ID
03177
International Designator
1968-026C
Epoch
Fri, 17 Jul 2026 00:40:05 GMT
Apogee
Calculating...
Perigee
Calculating...
Inclination
99.96°
Right Ascension
19.69°
Eccentricity
Calculating...
Argument of Perigee
256.00°
Period
206.25 min
Mean Motion
6.98 rev/day
Latitude
Calculating...
Longitude
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Altitude
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Velocity
Calculating...
Polar Plot
3D Visualization
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Basic Satellite Info
Name
OV1-14 R/B
Alternative Name
OV1-14P
Type
Rocket Body
Status
Space Junk
Owner
OAR
Country
United States
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 03177U 68026C 26198.02783882 -.00000039 00000+0 -34546-4 0 9993
2 03177 99.9605 19.6927 4013282 255.9979 321.8114 06.98172826479287
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
0.7
Span
2.1
Dry Mass
125
Launch Mass
125
Shape
Cyl
Radar Cross Section
0.92
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
FW4S
Purpose
Unknown
Mission
Unknown
Manufacturer
UTC
Life Expectancy
Unknown
Bus
FW4
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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