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 26140.55648847 +.00000000 +00000-0 +00000-0 0 00004
2 40746 0.0129 328.5791 0000082 80.2982 204.6933 1.00271333 06
| Epoch (UTC): | 20 May 2026 13:21:20 |
| Eccentricity: | 0.0000082 |
| inclination: | 0.0129° |
| perigee height: | 35786 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 328.5791° |
| argument of perigee: | 80.2982° |
| revolutions per day: | 1.00271333 |
| mean anomaly at epoch: | 204.6933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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