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 53106U 22080B 25167.32760529 -.00000003 00000-0 00000-0 0 9996
2 53106 70.1560 65.9804 0008358 24.6429 335.4629 6.42557409 68669
| Epoch (UTC): | 16 June 2025 07:51:45 |
| Eccentricity: | 0.0008358 |
| inclination: | 70.1560° |
| perigee height: | 5833 km |
| apogee height: | 5853 km |
| right ascension of ascending node: | 65.9804° |
| argument of perigee: | 24.6429° |
| revolutions per day: | 6.42557409 |
| mean anomaly at epoch: | 335.4629° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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