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 20691U 90050C 25194.31696772 .00007037 00000-0 52518-3 0 9995
2 20691 63.2966 43.8126 0889863 78.6833 291.2743 13.59508838 60175
| Epoch (UTC): | 13 July 2025 07:36:26 |
| Eccentricity: | 0.0889863 |
| inclination: | 63.2966° |
| perigee height: | 377 km |
| apogee height: | 1697 km |
| right ascension of ascending node: | 43.8126° |
| argument of perigee: | 78.6833° |
| revolutions per day: | 13.59508838 |
| mean anomaly at epoch: | 291.2743° |
| orbit number at epoch: | 6017 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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