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 55925U 26145.22725352 +.00000000 +00000-0 -72387-5 0 00008
2 55925 69.9993 111.4036 0003259 268.5719 91.5067 14.98330758 02
| Epoch (UTC): | 25 May 2026 05:27:14 |
| Eccentricity: | 0.0003259 |
| inclination: | 69.9993° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 111.4036° |
| argument of perigee: | 268.5719° |
| revolutions per day: | 14.98330758 |
| mean anomaly at epoch: | 91.5067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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