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 56809U 26145.46137042 +.00000000 +00000-0 -92725-5 0 00007
2 56809 69.9986 150.7355 0003644 265.2109 94.8634 14.98330946 06
| Epoch (UTC): | 25 May 2026 11:04:22 |
| Eccentricity: | 0.0003644 |
| inclination: | 69.9986° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 150.7355° |
| argument of perigee: | 265.2109° |
| revolutions per day: | 14.98330946 |
| mean anomaly at epoch: | 94.8634° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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