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 47351U 26145.59944258 +.00000000 +00000-0 -26349-5 0 00007
2 47351 53.1595 15.9504 0001061 87.9185 272.1937 15.31699968 08
| Epoch (UTC): | 25 May 2026 14:23:11 |
| Eccentricity: | 0.0001061 |
| inclination: | 53.1595° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 15.9504° |
| argument of perigee: | 87.9185° |
| revolutions per day: | 15.31699968 |
| mean anomaly at epoch: | 272.1937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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