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 35970U 93036AVL 24355.88754585 .00036838 00000-0 29798-2 0 9999
2 35970 74.0243 193.0691 0020513 42.1638 318.1122 14.99433844815023
| Epoch (UTC): | 20 December 2024 21:18:03 |
| Eccentricity: | 0.0020513 |
| inclination: | 74.0243° |
| perigee height: | 554 km |
| apogee height: | 583 km |
| right ascension of ascending node: | 193.0691° |
| argument of perigee: | 42.1638° |
| revolutions per day: | 14.99433844 |
| mean anomaly at epoch: | 318.1122° |
| orbit number at epoch: | 81502 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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