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 56368U 26145.42011221 +.00000000 +00000-0 +00000-0 0 00002
2 56368 0.0653 358.1223 0006714 66.0660 295.8806 5.00116534 03
| Epoch (UTC): | 25 May 2026 10:04:57 |
| Eccentricity: | 0.0006714 |
| inclination: | 0.0653° |
| perigee height: | 8056 km |
| apogee height: | 8076 km |
| right ascension of ascending node: | 358.1223° |
| argument of perigee: | 66.0660° |
| revolutions per day: | 5.00116534 |
| mean anomaly at epoch: | 295.8806° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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