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 32791U 08021J 23277.46281773 .00012669 00000-0 10683-2 0 9996
2 32791 97.6687 246.5768 0013381 54.4121 305.8346 14.98229804838014
| Epoch (UTC): | 04 October 2023 11:06:27 |
| Eccentricity: | 0.0013381 |
| inclination: | 97.6687° |
| perigee height: | 563 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 246.5768° |
| argument of perigee: | 54.4121° |
| revolutions per day: | 14.98229804 |
| mean anomaly at epoch: | 305.8346° |
| orbit number at epoch: | 83801 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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