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 20104U 89050B 25196.54680990 .00000112 00000-0 96732-4 0 9998
2 20104 82.9578 141.7119 0042880 197.7722 162.1938 13.77581599810531
| Epoch (UTC): | 15 July 2025 13:07:24 |
| Eccentricity: | 0.0042880 |
| inclination: | 82.9578° |
| perigee height: | 941 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 141.7119° |
| argument of perigee: | 197.7722° |
| revolutions per day: | 13.77581599 |
| mean anomaly at epoch: | 162.1938° |
| orbit number at epoch: | 81053 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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