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 26146.26006292 +.00000000 +00000-0 +00000-0 0 00000
2 40746 0.0104 76.5426 0000308 82.4736 353.4473 1.00271950 03
| Epoch (UTC): | 26 May 2026 06:14:29 |
| Eccentricity: | 0.0000308 |
| inclination: | 0.0104° |
| perigee height: | 35785 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 76.5426° |
| argument of perigee: | 82.4736° |
| revolutions per day: | 1.00271950 |
| mean anomaly at epoch: | 353.4473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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