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 55946U 26145.27292461 +.00000000 +00000-0 +85441-4 0 00009
2 55946 69.9998 91.2837 0002998 273.1807 86.9009 14.98340589 00
| Epoch (UTC): | 25 May 2026 06:33:00 |
| Eccentricity: | 0.0002998 |
| inclination: | 69.9998° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 91.2837° |
| argument of perigee: | 273.1807° |
| revolutions per day: | 14.98340589 |
| mean anomaly at epoch: | 86.9009° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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