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 40746U 26145.26193240 +.00000000 +00000-0 +00000-0 0 00009
2 40746 0.0093 69.7364 0000366 76.8389 5.5794 1.00271596 07
| Epoch (UTC): | 25 May 2026 06:17:10 |
| Eccentricity: | 0.0000366 |
| inclination: | 0.0093° |
| perigee height: | 35785 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 69.7364° |
| argument of perigee: | 76.8389° |
| revolutions per day: | 1.00271596 |
| mean anomaly at epoch: | 5.5794° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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