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 56724U 26145.36497060 +.00000000 +00000-0 -15278-3 0 00007
2 56724 87.8989 263.7508 0001901 73.5629 286.5710 13.15547244 04
| Epoch (UTC): | 25 May 2026 08:45:33 |
| Eccentricity: | 0.0001901 |
| inclination: | 87.8989° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7508° |
| argument of perigee: | 73.5629° |
| revolutions per day: | 13.15547244 |
| mean anomaly at epoch: | 286.5710° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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