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 40345U 26144.95991666 +.00000000 +00000-0 +00000-0 0 00007
2 40345 0.0132 273.8398 0000418 241.1874 163.0465 1.00272068 05
| Epoch (UTC): | 24 May 2026 23:02:16 |
| Eccentricity: | 0.0000418 |
| inclination: | 0.0132° |
| perigee height: | 35785 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 273.8398° |
| argument of perigee: | 241.1874° |
| revolutions per day: | 1.00272068 |
| mean anomaly at epoch: | 163.0465° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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