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 63186U 26145.55193840 +.00000000 +00000-0 +17948-2 0 00001
2 63186 43.0007 216.2344 0001060 280.4908 79.5840 15.70887544 02
| Epoch (UTC): | 25 May 2026 13:14:47 |
| Eccentricity: | 0.0001060 |
| inclination: | 43.0007° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 216.2344° |
| argument of perigee: | 280.4908° |
| revolutions per day: | 15.70887544 |
| mean anomaly at epoch: | 79.5840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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