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 24280.74608553 .00000178 00000-0 14120-3 0 9994
2 00058 28.3282 37.7182 0164773 126.8455 234.7321 13.46387373150651
| Epoch (UTC): | 06 October 2024 17:54:21 |
| Eccentricity: | 0.0164773 |
| inclination: | 28.3282° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 37.7182° |
| argument of perigee: | 126.8455° |
| revolutions per day: | 13.46387373 |
| mean anomaly at epoch: | 234.7321° |
| orbit number at epoch: | 15065 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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