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 56398U 26145.63326539 +.00000000 +00000-0 +18603-4 0 00001
2 56398 43.0050 112.3688 0001684 267.0125 93.0534 15.27577345 06
| Epoch (UTC): | 25 May 2026 15:11:54 |
| Eccentricity: | 0.0001684 |
| inclination: | 43.0050° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 112.3688° |
| argument of perigee: | 267.0125° |
| revolutions per day: | 15.27577345 |
| mean anomaly at epoch: | 93.0534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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