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 56814U 26145.33202499 +.00000000 +00000-0 -10878-4 0 00006
2 56814 69.9983 151.0859 0003609 261.6952 98.3798 14.98331316 01
| Epoch (UTC): | 25 May 2026 07:58:06 |
| Eccentricity: | 0.0003609 |
| inclination: | 69.9983° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 151.0859° |
| argument of perigee: | 261.6952° |
| revolutions per day: | 14.98331316 |
| mean anomaly at epoch: | 98.3798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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