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 47817U 26145.57648897 +.00000000 +00000-0 +24792-4 0 00000
2 47817 53.1567 245.5224 0001132 88.3078 271.8053 15.31701887 08
| Epoch (UTC): | 25 May 2026 13:50:08 |
| Eccentricity: | 0.0001132 |
| inclination: | 53.1567° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 245.5224° |
| argument of perigee: | 88.3078° |
| revolutions per day: | 15.31701887 |
| mean anomaly at epoch: | 271.8053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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