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 data is extracted from the following two-line orbital elements,
1 22566U 93016B 25188.59648534 .00000077 00000-0 63992-4 0 9995
2 22566 71.0086 9.9316 0011406 326.4452 33.5947 14.15264798667491
| Epoch (UTC): | 07 July 2025 14:18:56 |
| Eccentricity: | 0.0011406 |
| inclination: | 71.0086° |
| perigee height: | 833 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 9.9316° |
| argument of perigee: | 326.4452° |
| revolutions per day: | 14.15264798 |
| mean anomaly at epoch: | 33.5947° |
| orbit number at epoch: | 66749 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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