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 22177.87583880 .00000056 00000-0 37239-4 0 9991
2 20442 98.7942 142.8812 0012463 137.0074 223.2085 14.33066490694453
| Epoch (UTC): | 26 June 2022 21:01:12 |
| Eccentricity: | 0.0012463 |
| inclination: | 98.7942° |
| perigee height: | 772 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 142.8812° |
| argument of perigee: | 137.0074° |
| revolutions per day: | 14.33066490 |
| mean anomaly at epoch: | 223.2085° |
| orbit number at epoch: | 69445 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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