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 40946U 26145.52171417 +.00000000 +00000-0 +00000-0 0 00002
2 40946 3.1693 14.4611 0002172 358.1762 305.1938 1.00272225 08
| Epoch (UTC): | 25 May 2026 12:31:16 |
| Eccentricity: | 0.0002172 |
| inclination: | 3.1693° |
| perigee height: | 35777 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 14.4611° |
| argument of perigee: | 358.1762° |
| revolutions per day: | 1.00272225 |
| mean anomaly at epoch: | 305.1938° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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