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 22566U 26159.03452177 +.00000000 +00000-0 +69830-4 0 00006
2 22566 71.0079 25.4318 0010835 196.7781 163.2985 14.15308871 08
| Epoch (UTC): | 08 June 2026 00:49:42 |
| Eccentricity: | 0.0010835 |
| inclination: | 71.0079° |
| perigee height: | 833 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 25.4318° |
| argument of perigee: | 196.7781° |
| revolutions per day: | 14.15308871 |
| mean anomaly at epoch: | 163.2985° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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