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 40882U 26144.76377021 +.00000000 +00000-0 +00000-0 0 00005
2 40882 0.0165 337.5643 0000409 68.4838 290.8572 1.00272017 00
| Epoch (UTC): | 24 May 2026 18:19:49 |
| Eccentricity: | 0.0000409 |
| inclination: | 0.0165° |
| perigee height: | 35785 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 337.5643° |
| argument of perigee: | 68.4838° |
| revolutions per day: | 1.00272017 |
| mean anomaly at epoch: | 290.8572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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