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 40982U 26145.61187280 +.00000000 +00000-0 +00000-0 0 00007
2 40982 0.0593 62.5358 0001573 121.2899 61.6545 1.00270561 08
| Epoch (UTC): | 25 May 2026 14:41:05 |
| Eccentricity: | 0.0001573 |
| inclination: | 0.0593° |
| perigee height: | 35780 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 62.5358° |
| argument of perigee: | 121.2899° |
| revolutions per day: | 1.00270561 |
| mean anomaly at epoch: | 61.6545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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