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 23341.50381703 .00000227 00000-0 98978-4 0 9992
2 20442 98.8653 321.9178 0012452 35.0431 325.1570 14.33385431770174
| Epoch (UTC): | 07 December 2023 12:05:29 |
| Eccentricity: | 0.0012452 |
| inclination: | 98.8653° |
| perigee height: | 771 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 321.9178° |
| argument of perigee: | 35.0431° |
| revolutions per day: | 14.33385431 |
| mean anomaly at epoch: | 325.1570° |
| orbit number at epoch: | 77017 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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