Demystifying the USSPACECOM Two-Line Element Set Format
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ICEYE-X31 (58288)
COSPAR: 2023-174AJ | Alt Name: ICEYE-X31
Image
Additional Sources
Launch Details
Orbital Elements
NORAD ID
58288
International Designator
2023-174AJ
Epoch
Mon, 20 Jul 2026 06:09:03 GMT
Apogee
Calculating...
Perigee
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Inclination
97.38°
Right Ascension
277.01°
Eccentricity
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Argument of Perigee
172.70°
Period
93.79 min
Mean Motion
15.35 rev/day
Latitude
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Longitude
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Altitude
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Velocity
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Polar Plot
3D Visualization
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Basic Satellite Info
Name
ICEYE-X31
Alternative Name
ICEYE-X31
Type
Payload
Status
Operational
Owner
ICEYE
Country
Finland
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 58288U 23174AJ 26201.25628589 .00010108 00000+0 29736-3 0 9993
2 58288 97.3763 277.0087 0003208 172.7021 187.4270 15.35274337149825
Source: Celestrak
Summary
The ICEYE-X31 satellite, designated NORAD_CAT_ID 58288 and OBJECT_ID 2023-174AJ, was launched on November 11, 2023, from AFWTR SLC4E using a Falcon 9 launch vehicle. It is owned by ICEYE, the same company that manufactured it. The satellite has dimensions of 0.7 meters in length, 0.5 meters in diameter, and a span of 3.25 meters. Its dry mass is 89 kilograms while its launch mass was 90 kilograms. Equipped with X-band SAR (Synthetic Aperture Radar), ICEYE-X31 uses two deployable solar arrays for power generation along with batteries. The satellite's shape consists of a box structure augmented by a pan configuration, though specific details such as the mission and major events are not provided in the data.
Physical Characteristics
Length
0.7
Diameter
0.5
Span
3.25
Dry Mass
89
Launch Mass
90
Shape
Box + pan
Radar Cross Section
Unknown
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
ICEYE-X31
Purpose
Unknown
Mission
Unknown
Manufacturer
ICEYE
Life Expectancy
Unknown
Bus
ICEYE
Configuration
Unknown
Motor
?
Equipment
X-band SAR
Power System
2 deployable solar arrays, 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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