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 56355U 26145.66668980 +.00000000 +00000-0 -16957-3 0 00006
2 56355 97.5229 145.8937 0001669 93.6662 123.9117 15.22736834 06
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001669 |
| inclination: | 97.5229° |
| perigee height: | 496 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 145.8937° |
| argument of perigee: | 93.6662° |
| revolutions per day: | 15.22736834 |
| mean anomaly at epoch: | 123.9117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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