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 47895U 26144.67368862 +.00000000 +00000-0 +33183-3 0 00000
2 47895 53.1591 274.7547 0001155 74.2902 285.8227 15.31735786 01
| Epoch (UTC): | 24 May 2026 16:10:06 |
| Eccentricity: | 0.0001155 |
| inclination: | 53.1591° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 274.7547° |
| argument of perigee: | 74.2902° |
| revolutions per day: | 15.31735786 |
| mean anomaly at epoch: | 285.8227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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