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 56459U 26145.42584060 +.00000000 +00000-0 +45625-4 0 00005
2 56459 69.9995 310.8437 0002944 264.7690 95.3133 14.98331995 03
| Epoch (UTC): | 25 May 2026 10:13:12 |
| Eccentricity: | 0.0002944 |
| inclination: | 69.9995° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 310.8437° |
| argument of perigee: | 264.7690° |
| revolutions per day: | 14.98331995 |
| mean anomaly at epoch: | 95.3133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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