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 38147U 99025EQU 24355.77522775 .00002321 00000-0 10554-2 0 9994
2 38147 98.5800 13.6285 0050495 257.0030 102.5507 14.22040731553119
| Epoch (UTC): | 20 December 2024 18:36:19 |
| Eccentricity: | 0.0050495 |
| inclination: | 98.5800° |
| perigee height: | 782 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 13.6285° |
| argument of perigee: | 257.0030° |
| revolutions per day: | 14.22040731 |
| mean anomaly at epoch: | 102.5507° |
| orbit number at epoch: | 55311 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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