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DELTA 1 R/B(2) (02971)
COSPAR: 1967-094C | Alt Name: Unk US GTO object
Image
Additional Sources
Launch Details
Launch Date
September 28, 1967
Launch Site
Launch Pad
LC17B
Launch Vehicle
Thor Delta E1
Orbital Elements
NORAD ID
02971
International Designator
1967-094C
Epoch
Thu, 02 Jul 2026 05:00:45 GMT
Apogee
Calculating...
Perigee
Calculating...
Inclination
28.08°
Right Ascension
170.13°
Eccentricity
Calculating...
Argument of Perigee
130.62°
Period
445.96 min
Mean Motion
3.23 rev/day
Latitude
Calculating...
Longitude
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Altitude
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Velocity
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Polar Plot
3D Visualization
Basic Satellite Info
Name
DELTA 1 R/B(2)
Alternative Name
Unk US GTO object
Type
Rocket Body
Status
Space Junk
Owner
GSFC
Country
United States
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 2971U 67094C 26183.20885929 .00003092 00000-0 14849-2 0 9990
2 2971 28.0822 170.1283 6541496 130.6228 307.8886 3.22901553560317
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
1.5
Diameter
0.5
Span
1.5
Dry Mass
40
Launch Mass
40
Shape
Cyl
Radar Cross Section
1.572
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
[UNID016] RCS 1.2
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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