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 6393U 73015B 24357.98885387 .00000268 00000-0 15486-3 0 9997
2 6393 81.2543 181.2234 0059222 121.8369 238.8584 14.05321459652585
| Epoch (UTC): | 22 December 2024 23:43:56 |
| Eccentricity: | 0.0059222 |
| inclination: | 81.2543° |
| perigee height: | 832 km |
| apogee height: | 918 km |
| right ascension of ascending node: | 181.2234° |
| argument of perigee: | 121.8369° |
| revolutions per day: | 14.05321459 |
| mean anomaly at epoch: | 238.8584° |
| orbit number at epoch: | 65258 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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