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 40545U 26143.83209139 +.00000000 +00000-0 +00000-0 0 00002
2 40545 56.8011 342.2776 0001795 265.4418 94.5573 1.70475655 07
| Epoch (UTC): | 23 May 2026 19:58:12 |
| Eccentricity: | 0.0001795 |
| inclination: | 56.8011° |
| perigee height: | 23217 km |
| apogee height: | 23227 km |
| right ascension of ascending node: | 342.2776° |
| argument of perigee: | 265.4418° |
| revolutions per day: | 1.70475655 |
| mean anomaly at epoch: | 94.5573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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