Artemis II
Four astronauts, a patched-together heat shield, and a $50 billion question: whether NASA can still send humans beyond low Earth orbit. Tomorrow, we find out.
THOR ALTAIR R/B (01583)
COSPAR: 1965-072D | Alt Name: Thor Burner 1 (2) Stage 2
Image
Additional Sources
Launch Details
Launch Date
September 10, 1965
Launch Site
AFWTR
Launch Pad
4300B6
Launch Vehicle
Thor Burner 1
Orbital Elements
NORAD ID
01583
International Designator
1965-072D
Epoch
Sat, 04 Jul 2026 02:31:50 GMT
Apogee
Calculating...
Perigee
Calculating...
Inclination
98.39°
Right Ascension
60.13°
Eccentricity
Calculating...
Argument of Perigee
179.73°
Period
98.29 min
Mean Motion
14.65 rev/day
Latitude
Calculating...
Longitude
Calculating...
Altitude
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Velocity
Calculating...
Polar Plot
3D Visualization
Basic Satellite Info
Name
THOR ALTAIR R/B
Alternative Name
Thor Burner 1 (2) Stage 2
Type
Rocket Body
Status
Space Junk
Owner
AFSSD
Country
United States
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 01583U 65072D 26185.10544431 .00001518 00000-0 25431-3 0 9994
2 01583 98.3870 60.1349 0139655 179.7339 180.3963 14.65106839169420
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
25
Launch Mass
25
Shape
Cyl
Radar Cross Section
0.654
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
FW4S S/N 20032
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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