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 00058U 60013A 25138.73901500 .00000122 00000-0 52495-4 0 9991
2 00058 28.3296 341.1983 0164893 181.6012 178.4014 13.46410894180862
Epoch (UTC): | 18 May 2025 17:44:10 |
Eccentricity: | 0.0164893 |
inclination: | 28.3296° |
perigee height: | 962 km |
apogee height: | 1208 km |
right ascension of ascending node: | 341.1983° |
argument of perigee: | 181.6012° |
revolutions per day: | 13.46410894 |
mean anomaly at epoch: | 178.4014° |
orbit number at epoch: | 18086 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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