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 57646U 26145.33860219 +.00000000 +00000-0 -10006-4 0 00003
2 57646 43.0051 19.2683 0001372 273.6349 86.4346 15.27588839 06
| Epoch (UTC): | 25 May 2026 08:07:35 |
| Eccentricity: | 0.0001372 |
| inclination: | 43.0051° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 19.2683° |
| argument of perigee: | 273.6349° |
| revolutions per day: | 15.27588839 |
| mean anomaly at epoch: | 86.4346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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