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 47815U 26145.54846961 +.00000000 +00000-0 +35541-3 0 00000
2 47815 53.1591 245.2176 0001370 80.1899 279.9257 15.31697196 03
| Epoch (UTC): | 25 May 2026 13:09:47 |
| Eccentricity: | 0.0001370 |
| inclination: | 53.1591° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 245.2176° |
| argument of perigee: | 80.1899° |
| revolutions per day: | 15.31697196 |
| mean anomaly at epoch: | 279.9257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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