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 24314.11173387 .00000201 00000-0 18045-3 0 9992
2 58 28.3264 228.4323 0164814 43.1827 318.1515 13.46393988155697
Epoch (UTC): | 09 November 2024 02:40:53 |
Eccentricity: | 0.0164814 |
inclination: | 28.3264° |
perigee height: | 962 km |
apogee height: | 1208 km |
right ascension of ascending node: | 228.4323° |
argument of perigee: | 43.1827° |
revolutions per day: | 13.46393988 |
mean anomaly at epoch: | 318.1515° |
orbit number at epoch: | 15569 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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