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 24255.46151917 .00000140 00000-0 79865-4 0 9999
2 58 28.3277 166.0098 0164903 277.4831 80.7007 13.46384621147786
| Epoch (UTC): | 11 September 2024 11:04:35 |
| Eccentricity: | 0.0164903 |
| inclination: | 28.3277° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 166.0098° |
| argument of perigee: | 277.4831° |
| revolutions per day: | 13.46384621 |
| mean anomaly at epoch: | 80.7007° |
| orbit number at epoch: | 14778 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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