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 47650U 26145.43103197 +.00000000 +00000-0 +13130-2 0 00001
2 47650 53.1508 50.2864 0005717 87.4933 272.6726 15.38889853 05
| Epoch (UTC): | 25 May 2026 10:20:41 |
| Eccentricity: | 0.0005717 |
| inclination: | 53.1508° |
| perigee height: | 445 km |
| apogee height: | 453 km |
| right ascension of ascending node: | 50.2864° |
| argument of perigee: | 87.4933° |
| revolutions per day: | 15.38889853 |
| mean anomaly at epoch: | 272.6726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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