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 25194.02274477 .00007143 00000-0 53287-3 0 9999
2 20691 63.2966 44.6022 0889880 78.6779 291.2796 13.59504718 60112
| Epoch (UTC): | 13 July 2025 00:32:45 |
| Eccentricity: | 0.0889880 |
| inclination: | 63.2966° |
| perigee height: | 377 km |
| apogee height: | 1697 km |
| right ascension of ascending node: | 44.6022° |
| argument of perigee: | 78.6779° |
| revolutions per day: | 13.59504718 |
| mean anomaly at epoch: | 291.2796° |
| orbit number at epoch: | 6011 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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