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 43189U 18014K 25341.01605727 .00010573 00000-0 58154-3 0 9994
2 43189 97.5518 242.3504 0009616 321.1548 38.8991 15.14214176428204
| Epoch (UTC): | 07 December 2025 00:23:07 |
| Eccentricity: | 0.0009616 |
| inclination: | 97.5518° |
| perigee height: | 517 km |
| apogee height: | 530 km |
| right ascension of ascending node: | 242.3504° |
| argument of perigee: | 321.1548° |
| revolutions per day: | 15.14214176 |
| mean anomaly at epoch: | 38.8991° |
| orbit number at epoch: | 42820 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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