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 56450U 26145.45506194 +.00000000 +00000-0 -94518-4 0 00007
2 56450 69.9991 310.9479 0002642 271.0434 89.0423 14.98331027 07
| Epoch (UTC): | 25 May 2026 10:55:17 |
| Eccentricity: | 0.0002642 |
| inclination: | 69.9991° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 310.9479° |
| argument of perigee: | 271.0434° |
| revolutions per day: | 14.98331027 |
| mean anomaly at epoch: | 89.0423° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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