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 57068U 26145.40900223 +.00000000 +00000-0 -98306-4 0 00008
2 57068 43.0043 40.9640 0001040 259.6179 100.4556 15.27590982 08
| Epoch (UTC): | 25 May 2026 09:48:57 |
| Eccentricity: | 0.0001040 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 40.9640° |
| argument of perigee: | 259.6179° |
| revolutions per day: | 15.27590982 |
| mean anomaly at epoch: | 100.4556° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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