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 23336.47609372 .00026209 00000-0 21286-2 0 9998
2 32791 97.6814 304.6684 0009113 190.1167 169.9874 14.99554094846933
| Epoch (UTC): | 02 December 2023 11:25:34 |
| Eccentricity: | 0.0009113 |
| inclination: | 97.6814° |
| perigee height: | 562 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 304.6684° |
| argument of perigee: | 190.1167° |
| revolutions per day: | 14.99554094 |
| mean anomaly at epoch: | 169.9874° |
| orbit number at epoch: | 84693 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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