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 56495U 26145.39183554 +.00000000 +00000-0 +79351-5 0 00008
2 56495 69.9991 270.9816 0003067 270.7977 89.2831 14.98328208 08
| Epoch (UTC): | 25 May 2026 09:24:14 |
| Eccentricity: | 0.0003067 |
| inclination: | 69.9991° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 270.9816° |
| argument of perigee: | 270.7977° |
| revolutions per day: | 14.98328208 |
| mean anomaly at epoch: | 89.2831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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