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 24357.93784378 .00000471 00000-0 18625-3 0 9993
2 20442 98.8950 353.3323 0011625 358.2013 1.9127 14.33801478824881
| Epoch (UTC): | 22 December 2024 22:30:29 |
| Eccentricity: | 0.0011625 |
| inclination: | 98.8950° |
| perigee height: | 771 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 353.3323° |
| argument of perigee: | 358.2013° |
| revolutions per day: | 14.33801478 |
| mean anomaly at epoch: | 1.9127° |
| orbit number at epoch: | 82488 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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