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 47533U 26145.59852779 +.00000000 +00000-0 -12046-3 0 00002
2 47533 63.4023 200.1775 0174461 0.5479 359.5707 13.45446151 02
| Epoch (UTC): | 25 May 2026 14:21:52 |
| Eccentricity: | 0.0174461 |
| inclination: | 63.4023° |
| perigee height: | 959 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 200.1775° |
| argument of perigee: | 0.5479° |
| revolutions per day: | 13.45446151 |
| mean anomaly at epoch: | 359.5707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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