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 20442U 90005G 25013.43115620 .00000336 00000-0 13766-3 0 9997
2 20442 98.8960 15.4244 0010660 291.9984 68.0067 14.33828775827966
| Epoch (UTC): | 13 January 2025 10:20:51 |
| Eccentricity: | 0.0010660 |
| inclination: | 98.8960° |
| perigee height: | 771 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 15.4244° |
| argument of perigee: | 291.9984° |
| revolutions per day: | 14.33828775 |
| mean anomaly at epoch: | 68.0067° |
| orbit number at epoch: | 82796 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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