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THEMIS E (30798)
COSPAR: 2007-004E | Alt Name: THEMIS E
Image
Additional Sources
Launch Details
Launch Date
February 17, 2007
Launch Site
Launch Pad
SLC17B
Launch Vehicle
Delta 7925-10C
Orbital Elements
NORAD ID
30798
International Designator
2007-004E
Epoch
Fri, 03 Jul 2026 23:29:48 GMT
Apogee
Calculating...
Perigee
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Inclination
6.53°
Right Ascension
97.09°
Eccentricity
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Argument of Perigee
218.55°
Period
1635.59 min
Mean Motion
0.88 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
THEMIS E
Alternative Name
THEMIS E
Type
Payload
Status
Operational
Owner
GSFC
Country
United States
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 30798U 07004E 26184.97903470 -.00000400 00000-0 00000-0 0 9993
2 30798 6.5283 97.0944 8437049 218.5458 13.1584 0.88041892 66064
Source: Celestrak
Summary
THEMIS E is a research satellite launched on February 17, 2007, from Cape Canaveral Air Force Station, SLC17B, using the Delta 7925-10C launch vehicle. It has dimensions of 0.5 meters in length and 0.8 meters in diameter with a span of 49.6 meters. The satellite's dry mass is 76 kilograms, and it had a launch mass of 125 kilograms. Equipped with solar cells and batteries for power generation, THEMIS E was designed to operate for approximately two years and is owned by GSFC (Goddard Space Flight Center). Manufactured by SWALES, the spacecraft has a configuration known as SMEX-Lite and features a box shape augmented with two antennas. Its mission involved research purposes, and it was part of the THEMIS P4 payload system.
Physical Characteristics
Length
0.5
Diameter
0.8
Span
49.6
Dry Mass
76
Launch Mass
125
Shape
Box + 2 Ant
Radar Cross Section
0.6325
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
THEMIS P4
Purpose
Research
Mission
Research
Manufacturer
SWALES
Life Expectancy
2 years
Bus
ATK-A100
Configuration
SMEX-Lite Spacecraft
Motor
Unknown
Equipment
see above
Power System
Solar cells, batteries
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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