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 56790U 26145.31905748 +.00000000 +00000-0 +27414-4 0 00007
2 56790 69.9993 111.2929 0003259 267.1455 92.9331 14.98337792 08
| Epoch (UTC): | 25 May 2026 07:39:26 |
| Eccentricity: | 0.0003259 |
| inclination: | 69.9993° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 111.2929° |
| argument of perigee: | 267.1455° |
| revolutions per day: | 14.98337792 |
| mean anomaly at epoch: | 92.9331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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