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 20438U 90005C 21342.61925288 -.00000009 00000-0 14130-4 0 9997
2 20438 98.9196 336.1432 0010647 130.0682 345.2678 14.31094917663954
| Epoch (UTC): | 08 December 2021 14:51:43 |
| Eccentricity: | 0.0010647 |
| inclination: | 98.9196° |
| perigee height: | 780 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 336.1432° |
| argument of perigee: | 130.0682° |
| revolutions per day: | 14.31094917 |
| mean anomaly at epoch: | 345.2678° |
| orbit number at epoch: | 66395 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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