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 47532U 26145.59849457 +.00000000 +00000-0 -15213-3 0 00009
2 47532 63.4029 201.1698 0173986 0.4351 359.6796 13.45446015 09
| Epoch (UTC): | 25 May 2026 14:21:49 |
| Eccentricity: | 0.0173986 |
| inclination: | 63.4029° |
| perigee height: | 959 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 201.1698° |
| argument of perigee: | 0.4351° |
| revolutions per day: | 13.45446015 |
| mean anomaly at epoch: | 359.6796° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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