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 24262.80224379 .00000126 00000-0 63005-4 0 9991
2 58 28.3271 128.7640 0164828 338.2594 21.1020 13.46385204148778
Epoch (UTC): | 18 September 2024 19:15:13 |
Eccentricity: | 0.0164828 |
inclination: | 28.3271° |
perigee height: | 962 km |
apogee height: | 1208 km |
right ascension of ascending node: | 128.7640° |
argument of perigee: | 338.2594° |
revolutions per day: | 13.46385204 |
mean anomaly at epoch: | 21.1020° |
orbit number at epoch: | 14877 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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