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 56996U 23084BY 24358.09491102 .00006718 00000-0 86212-3 0 9994
2 56996 98.0811 118.7709 0063790 53.4858 307.2205 14.80118430 73172
| Epoch (UTC): | 23 December 2024 02:16:40 |
| Eccentricity: | 0.0063790 |
| inclination: | 98.0811° |
| perigee height: | 584 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 118.7709° |
| argument of perigee: | 53.4858° |
| revolutions per day: | 14.80118430 |
| mean anomaly at epoch: | 307.2205° |
| orbit number at epoch: | 7317 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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