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 55746U 26145.48108542 +.00000000 +00000-0 +16380-4 0 00002
2 55746 70.0008 50.8054 0002645 270.4361 89.6495 14.98330113 00
| Epoch (UTC): | 25 May 2026 11:32:45 |
| Eccentricity: | 0.0002645 |
| inclination: | 70.0008° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 50.8054° |
| argument of perigee: | 270.4361° |
| revolutions per day: | 14.98330113 |
| mean anomaly at epoch: | 89.6495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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