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 31826U 99025CHQ 24357.46713080 .00001125 00000-0 52360-3 0 9993
2 31826 98.6060 352.4799 0126465 133.9882 18.4420 14.18258631907765
| Epoch (UTC): | 22 December 2024 11:12:40 |
| Eccentricity: | 0.0126465 |
| inclination: | 98.6060° |
| perigee height: | 740 km |
| apogee height: | 922 km |
| right ascension of ascending node: | 352.4799° |
| argument of perigee: | 133.9882° |
| revolutions per day: | 14.18258631 |
| mean anomaly at epoch: | 18.4420° |
| orbit number at epoch: | 90776 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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