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 63011U 26145.54564958 +.00000000 +00000-0 +12687-2 0 00004
2 63011 43.0013 91.8607 0001374 290.6633 69.4088 15.70929177 02
| Epoch (UTC): | 25 May 2026 13:05:44 |
| Eccentricity: | 0.0001374 |
| inclination: | 43.0013° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 91.8607° |
| argument of perigee: | 290.6633° |
| revolutions per day: | 15.70929177 |
| mean anomaly at epoch: | 69.4088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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