View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 31123U 07012G 25189.62683866 .00000041 00000-0 29519-4 0 9995
2 31123 98.0573 63.7620 0309091 325.2245 53.0736 14.13402705939689
Epoch (UTC): | 08 July 2025 15:02:38 |
Eccentricity: | 0.0309091 |
inclination: | 98.0573° |
perigee height: | 624 km |
apogee height: | 1071 km |
right ascension of ascending node: | 63.7620° |
argument of perigee: | 325.2245° |
revolutions per day: | 14.13402705 |
mean anomaly at epoch: | 53.0736° |
orbit number at epoch: | 93968 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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