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 66027U 26145.58335647 +.00000000 +00000-0 -47586-3 0 00007
2 66027 53.1594 106.9957 0000855 92.5777 305.1802 15.33547390 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000855 |
| inclination: | 53.1594° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 106.9957° |
| argument of perigee: | 92.5777° |
| revolutions per day: | 15.33547390 |
| mean anomaly at epoch: | 305.1802° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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