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 56357U 26145.46761855 +.00000000 +00000-0 +59422-4 0 00005
2 56357 97.4482 146.5894 0001748 108.0713 252.0705 15.05650647 09
| Epoch (UTC): | 25 May 2026 11:13:22 |
| Eccentricity: | 0.0001748 |
| inclination: | 97.4482° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 146.5894° |
| argument of perigee: | 108.0713° |
| revolutions per day: | 15.05650647 |
| mean anomaly at epoch: | 252.0705° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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