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 58U 60013A 25197.83212140 .00000088 00000-0 40798-5 0 9997
2 58 28.3298 41.3594 0164910 310.8709 47.7651 13.46412931189374
Epoch (UTC): | 16 July 2025 19:58:15 |
Eccentricity: | 0.0164910 |
inclination: | 28.3298° |
perigee height: | 962 km |
apogee height: | 1208 km |
right ascension of ascending node: | 41.3594° |
argument of perigee: | 310.8709° |
revolutions per day: | 13.46412931 |
mean anomaly at epoch: | 47.7651° |
orbit number at epoch: | 18937 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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