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 56631U 22151AFF 24356.53964304 .00031728 00000-0 55343-2 0 9999
2 56631 98.6495 29.3862 0082928 143.0966 217.5982 14.65638340 87809
| Epoch (UTC): | 21 December 2024 12:57:05 |
| Eccentricity: | 0.0082928 |
| inclination: | 98.6495° |
| perigee height: | 616 km |
| apogee height: | 733 km |
| right ascension of ascending node: | 29.3862° |
| argument of perigee: | 143.0966° |
| revolutions per day: | 14.65638340 |
| mean anomaly at epoch: | 217.5982° |
| orbit number at epoch: | 8780 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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