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 40186U 11077K 25338.54532154 -.00000077 00000-0 00000+0 0 9999
2 40186 25.4688 133.1571 7307646 171.8762 229.0196 1.88729099 95444
| Epoch (UTC): | 04 December 2025 13:05:15 |
| Eccentricity: | 0.7307646 |
| inclination: | 25.4688° |
| perigee height: | 1069 km |
| apogee height: | 41493 km |
| right ascension of ascending node: | 133.1571° |
| argument of perigee: | 171.8762° |
| revolutions per day: | 1.88729099 |
| mean anomaly at epoch: | 229.0196° |
| orbit number at epoch: | 9544 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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