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 47780U 26145.55254249 +.00000000 +00000-0 +23175-4 0 00005
2 47780 53.1598 206.3374 0001326 90.6826 269.4327 15.31696481 04
| Epoch (UTC): | 25 May 2026 13:15:39 |
| Eccentricity: | 0.0001326 |
| inclination: | 53.1598° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 206.3374° |
| argument of perigee: | 90.6826° |
| revolutions per day: | 15.31696481 |
| mean anomaly at epoch: | 269.4327° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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