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 47873U 26145.02951796 +.00000000 +00000-0 -22040-4 0 00002
2 47873 53.1578 260.3637 0001844 79.5794 280.5415 15.31697140 07
| Epoch (UTC): | 25 May 2026 00:42:30 |
| Eccentricity: | 0.0001844 |
| inclination: | 53.1578° |
| perigee height: | 469 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 260.3637° |
| argument of perigee: | 79.5794° |
| revolutions per day: | 15.31697140 |
| mean anomaly at epoch: | 280.5415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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