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 is defined by the following mean orbital elements,
1 47026U 99025FBC 24197.98627178 .00005019 00000-0 29627-2 0 9998
2 47026 98.1791 269.3406 0078241 131.7472 229.0423 14.06656095698178
| Epoch (UTC): | 15 July 2024 23:40:13 |
| Eccentricity: | 0.0078241 |
| inclination: | 98.1791° |
| perigee height: | 814 km |
| apogee height: | 927 km |
| right ascension of ascending node: | 269.3406° |
| argument of perigee: | 131.7472° |
| revolutions per day: | 14.06656095 |
| mean anomaly at epoch: | 229.0423° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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