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 47916U 26145.28585433 +.00000000 +00000-0 +37822-4 0 00002
2 47916 53.1575 259.1717 0001145 86.5174 273.5958 15.31697573 05
| Epoch (UTC): | 25 May 2026 06:51:37 |
| Eccentricity: | 0.0001145 |
| inclination: | 53.1575° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 259.1717° |
| argument of perigee: | 86.5174° |
| revolutions per day: | 15.31697573 |
| mean anomaly at epoch: | 273.5958° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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