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 24254.71628634 .00007478 00000-0 10623-2 0 9991
2 39161 97.8205 318.5814 0007748 318.7216 41.3408 14.77182210609757
| Epoch (UTC): | 10 September 2024 17:11:27 |
| Eccentricity: | 0.0007748 |
| inclination: | 97.8205° |
| perigee height: | 633 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 318.5814° |
| argument of perigee: | 318.7216° |
| revolutions per day: | 14.77182210 |
| mean anomaly at epoch: | 41.3408° |
| orbit number at epoch: | 60975 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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