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 23333.47628626 .00000473 00000-0 18815-3 0 9991
2 20442 98.8645 313.7004 0012652 56.9998 303.2400 14.33378541769085
| Epoch (UTC): | 29 November 2023 11:25:51 |
| Eccentricity: | 0.0012652 |
| inclination: | 98.8645° |
| perigee height: | 771 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 313.7004° |
| argument of perigee: | 56.9998° |
| revolutions per day: | 14.33378541 |
| mean anomaly at epoch: | 303.2400° |
| orbit number at epoch: | 76908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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