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 56897U 26145.03781700 +.00000000 +00000-0 +63172-4 0 00005
2 56897 43.0057 17.7066 0001551 275.4509 84.6165 15.27582619 03
| Epoch (UTC): | 25 May 2026 00:54:27 |
| Eccentricity: | 0.0001551 |
| inclination: | 43.0057° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 17.7066° |
| argument of perigee: | 275.4509° |
| revolutions per day: | 15.27582619 |
| mean anomaly at epoch: | 84.6165° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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