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 24255.90640136 .00000131 00000-0 66600-4 0 9997
2 00058 28.3277 163.7525 0164894 281.1651 77.0398 13.46384619147303
| Epoch (UTC): | 11 September 2024 21:45:13 |
| Eccentricity: | 0.0164894 |
| inclination: | 28.3277° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 163.7525° |
| argument of perigee: | 281.1651° |
| revolutions per day: | 13.46384619 |
| mean anomaly at epoch: | 77.0398° |
| orbit number at epoch: | 14730 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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