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 56475U 26144.82879403 +.00000000 +00000-0 +10644-3 0 00006
2 56475 69.9987 292.4998 0002974 268.1828 91.8990 14.98338773 06
| Epoch (UTC): | 24 May 2026 19:53:27 |
| Eccentricity: | 0.0002974 |
| inclination: | 69.9987° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 292.4998° |
| argument of perigee: | 268.1828° |
| revolutions per day: | 14.98338773 |
| mean anomaly at epoch: | 91.8990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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