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 66250U 26145.64692889 +.00000000 +00000-0 +63687-3 0 00005
2 66250 53.1621 286.1036 0000454 163.2178 196.8838 15.31705205 08
| Epoch (UTC): | 25 May 2026 15:31:34 |
| Eccentricity: | 0.0000454 |
| inclination: | 53.1621° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 286.1036° |
| argument of perigee: | 163.2178° |
| revolutions per day: | 15.31705205 |
| mean anomaly at epoch: | 196.8838° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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