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 22180.80828780 .00000020 00000-0 23948-4 0 9992
2 20442 98.7944 145.8586 0012594 128.9472 231.2836 14.33066869694938
| Epoch (UTC): | 29 June 2022 19:23:56 |
| Eccentricity: | 0.0012594 |
| inclination: | 98.7944° |
| perigee height: | 772 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 145.8586° |
| argument of perigee: | 128.9472° |
| revolutions per day: | 14.33066869 |
| mean anomaly at epoch: | 231.2836° |
| orbit number at epoch: | 69493 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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