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 56471U 26145.37540655 +.00000000 +00000-0 +85900-4 0 00005
2 56471 69.9987 291.1991 0003253 264.9721 95.1067 14.98333309 00
| Epoch (UTC): | 25 May 2026 09:00:35 |
| Eccentricity: | 0.0003253 |
| inclination: | 69.9987° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 291.1991° |
| argument of perigee: | 264.9721° |
| revolutions per day: | 14.98333309 |
| mean anomaly at epoch: | 95.1067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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