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 40082U 26144.74499983 +.00000000 +00000-0 +00000-0 0 00007
2 40082 0.0493 350.1666 0002738 75.1067 294.7545 5.00116027 03
| Epoch (UTC): | 24 May 2026 17:52:47 |
| Eccentricity: | 0.0002738 |
| inclination: | 0.0493° |
| perigee height: | 8062 km |
| apogee height: | 8070 km |
| right ascension of ascending node: | 350.1666° |
| argument of perigee: | 75.1067° |
| revolutions per day: | 5.00116027 |
| mean anomaly at epoch: | 294.7545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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