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 56745U 26145.60658485 +.00000000 +00000-0 +53611-3 0 00009
2 56745 97.5275 353.8020 0006181 83.9455 276.2498 15.45561013 04
| Epoch (UTC): | 25 May 2026 14:33:28 |
| Eccentricity: | 0.0006181 |
| inclination: | 97.5275° |
| perigee height: | 426 km |
| apogee height: | 434 km |
| right ascension of ascending node: | 353.8020° |
| argument of perigee: | 83.9455° |
| revolutions per day: | 15.45561013 |
| mean anomaly at epoch: | 276.2498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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