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 06797U 73058B 24287.39528466 -.00000095 00000-0 45153-3 0 9994
2 06797 27.9089 29.3042 7207089 318.0430 5.2539 2.21817171413741
| Epoch (UTC): | 13 October 2024 09:29:12 |
| Eccentricity: | 0.7207089 |
| inclination: | 27.9089° |
| perigee height: | 558 km |
| apogee height: | 36356 km |
| right ascension of ascending node: | 29.3042° |
| argument of perigee: | 318.0430° |
| revolutions per day: | 2.21817171 |
| mean anomaly at epoch: | 5.2539° |
| orbit number at epoch: | 41374 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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