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 39161U 13021C 24252.41318051 .00007820 00000-0 11113-2 0 9991
2 39161 97.8208 316.3488 0007923 327.2237 32.8481 14.77150140609412
| Epoch (UTC): | 08 September 2024 09:54:58 |
| Eccentricity: | 0.0007923 |
| inclination: | 97.8208° |
| perigee height: | 633 km |
| apogee height: | 644 km |
| right ascension of ascending node: | 316.3488° |
| argument of perigee: | 327.2237° |
| revolutions per day: | 14.77150140 |
| mean anomaly at epoch: | 32.8481° |
| orbit number at epoch: | 60941 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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