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 57446C 23105S 24358.48034722 -.00024045 00000+0 -17748-2 0 3583
2 57446 43.0012 126.1142 0001376 270.4826 90.3673 15.02547984 15
| Epoch (UTC): | 23 December 2024 11:31:42 |
| Eccentricity: | 0.0001376 |
| inclination: | 43.0012° |
| perigee height: | 558 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 126.1142° |
| argument of perigee: | 270.4826° |
| revolutions per day: | 15.02547984 |
| mean anomaly at epoch: | 90.3673° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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