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 56943U 26145.51648176 +.00000000 +00000-0 +52752-3 0 00000
2 56943 97.4847 290.3045 0002249 303.1796 56.9251 15.71535422 00
| Epoch (UTC): | 25 May 2026 12:23:44 |
| Eccentricity: | 0.0002249 |
| inclination: | 97.4847° |
| perigee height: | 353 km |
| apogee height: | 356 km |
| right ascension of ascending node: | 290.3045° |
| argument of perigee: | 303.1796° |
| revolutions per day: | 15.71535422 |
| mean anomaly at epoch: | 56.9251° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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