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 57670U 26145.44818818 +.00000000 +00000-0 -18228-4 0 00004
2 57670 53.1597 210.5296 0001219 100.5480 259.5658 15.30181472 05
| Epoch (UTC): | 25 May 2026 10:45:23 |
| Eccentricity: | 0.0001219 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 210.5296° |
| argument of perigee: | 100.5480° |
| revolutions per day: | 15.30181472 |
| mean anomaly at epoch: | 259.5658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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