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 47430U 26145.57812690 +.00000000 +00000-0 +13269-2 0 00000
2 47430 97.2291 213.3241 0003689 234.7380 125.3541 15.76264830 02
| Epoch (UTC): | 25 May 2026 13:52:30 |
| Eccentricity: | 0.0003689 |
| inclination: | 97.2291° |
| perigee height: | 339 km |
| apogee height: | 344 km |
| right ascension of ascending node: | 213.3241° |
| argument of perigee: | 234.7380° |
| revolutions per day: | 15.76264830 |
| mean anomaly at epoch: | 125.3541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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