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 22179.48170386 .00000033 00000-0 28628-4 0 9990
2 20442 98.7943 144.5117 0012540 132.6005 227.6238 14.33066726694687
| Epoch (UTC): | 28 June 2022 11:33:39 |
| Eccentricity: | 0.0012540 |
| inclination: | 98.7943° |
| perigee height: | 772 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 144.5117° |
| argument of perigee: | 132.6005° |
| revolutions per day: | 14.33066726 |
| mean anomaly at epoch: | 227.6238° |
| orbit number at epoch: | 69468 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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