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 56806U 26145.28567438 +.00000000 +00000-0 +54540-4 0 00001
2 56806 69.9990 111.1758 0003225 265.3250 94.7541 14.98332104 03
| Epoch (UTC): | 25 May 2026 06:51:22 |
| Eccentricity: | 0.0003225 |
| inclination: | 69.9990° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 111.1758° |
| argument of perigee: | 265.3250° |
| revolutions per day: | 14.98332104 |
| mean anomaly at epoch: | 94.7541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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