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 31888U 99025CKP 24357.68622653 .00008426 00000-0 33570-2 0 9992
2 31888 99.1548 259.0986 0018700 159.2646 200.9297 14.28740225905574
| Epoch (UTC): | 22 December 2024 16:28:09 |
| Eccentricity: | 0.0018700 |
| inclination: | 99.1548° |
| perigee height: | 782 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 259.0986° |
| argument of perigee: | 159.2646° |
| revolutions per day: | 14.28740225 |
| mean anomaly at epoch: | 200.9297° |
| orbit number at epoch: | 90557 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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