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 22176.47943411 .00000055 00000-0 36578-4 0 9990
2 20442 98.7940 141.4634 0012386 140.8843 219.3238 14.33066110694251
| Epoch (UTC): | 25 June 2022 11:30:23 |
| Eccentricity: | 0.0012386 |
| inclination: | 98.7940° |
| perigee height: | 772 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 141.4634° |
| argument of perigee: | 140.8843° |
| revolutions per day: | 14.33066110 |
| mean anomaly at epoch: | 219.3238° |
| orbit number at epoch: | 69425 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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