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 24256.87031792 .00000133 00000-0 70844-4 0 9993
2 00058 28.3277 158.8618 0164887 289.1453 69.1310 13.46384748147434
| Epoch (UTC): | 12 September 2024 20:53:15 |
| Eccentricity: | 0.0164887 |
| inclination: | 28.3277° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 158.8618° |
| argument of perigee: | 289.1453° |
| revolutions per day: | 13.46384748 |
| mean anomaly at epoch: | 69.1310° |
| orbit number at epoch: | 14743 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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