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 56477U 26145.41309905 +.00000000 +00000-0 -62543-4 0 00006
2 56477 69.9986 290.9271 0002565 263.9983 96.0884 14.98335147 06
| Epoch (UTC): | 25 May 2026 09:54:51 |
| Eccentricity: | 0.0002565 |
| inclination: | 69.9986° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 290.9271° |
| argument of perigee: | 263.9983° |
| revolutions per day: | 14.98335147 |
| mean anomaly at epoch: | 96.0884° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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