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 47776U 26145.40365411 +.00000000 +00000-0 +10189-2 0 00007
2 47776 53.1550 196.7999 0006863 350.0056 10.0818 15.54184546 05
| Epoch (UTC): | 25 May 2026 09:41:15 |
| Eccentricity: | 0.0006863 |
| inclination: | 53.1550° |
| perigee height: | 400 km |
| apogee height: | 409 km |
| right ascension of ascending node: | 196.7999° |
| argument of perigee: | 350.0056° |
| revolutions per day: | 15.54184546 |
| mean anomaly at epoch: | 10.0818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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