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 66253U 26145.66093338 +.00000000 +00000-0 +71350-3 0 00000
2 66253 53.1597 286.1898 0000575 77.9227 282.1839 15.31746088 03
| Epoch (UTC): | 25 May 2026 15:51:44 |
| Eccentricity: | 0.0000575 |
| inclination: | 53.1597° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 286.1898° |
| argument of perigee: | 77.9227° |
| revolutions per day: | 15.31746088 |
| mean anomaly at epoch: | 282.1839° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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