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 56193U 26145.24372465 +.00000000 +00000-0 +20543-3 0 00005
2 56193 97.2760 31.4205 0003820 110.7880 249.3769 15.27079889 06
| Epoch (UTC): | 25 May 2026 05:50:57 |
| Eccentricity: | 0.0003820 |
| inclination: | 97.2760° |
| perigee height: | 482 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 31.4205° |
| argument of perigee: | 110.7880° |
| revolutions per day: | 15.27079889 |
| mean anomaly at epoch: | 249.3769° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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