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 is defined by the following mean orbital elements,
1 40718U 26145.58768450 +.00000000 +00000-0 +21713-3 0 00001
2 40718 97.6506 324.6033 0014849 14.7980 345.3666 14.83505875 00
| Epoch (UTC): | 25 May 2026 14:06:15 |
| Eccentricity: | 0.0014849 |
| inclination: | 97.6506° |
| perigee height: | 608 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 324.6033° |
| argument of perigee: | 14.7980° |
| revolutions per day: | 14.83505875 |
| mean anomaly at epoch: | 345.3666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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