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 40663U 26145.49208494 +.00000000 +00000-0 +00000-0 0 00000
2 40663 0.0173 338.5900 0000212 98.7807 239.9759 1.00272843 05
| Epoch (UTC): | 25 May 2026 11:48:36 |
| Eccentricity: | 0.0000212 |
| inclination: | 0.0173° |
| perigee height: | 35785 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 338.5900° |
| argument of perigee: | 98.7807° |
| revolutions per day: | 1.00272843 |
| mean anomaly at epoch: | 239.9759° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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