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 61568U 26145.58465177 +.00000000 +00000-0 +22789-3 0 00001
2 61568 88.9836 57.6358 0008707 100.1517 260.0660 14.28238716 03
| Epoch (UTC): | 25 May 2026 14:01:53 |
| Eccentricity: | 0.0008707 |
| inclination: | 88.9836° |
| perigee height: | 791 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 57.6358° |
| argument of perigee: | 100.1517° |
| revolutions per day: | 14.28238716 |
| mean anomaly at epoch: | 260.0660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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