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 22180.87810800 .00000020 00000-0 23977-4 0 9995
2 20442 98.7944 145.9295 0012598 128.7581 231.4730 14.33066884694885
| Epoch (UTC): | 29 June 2022 21:04:28 |
| Eccentricity: | 0.0012598 |
| inclination: | 98.7944° |
| perigee height: | 772 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 145.9295° |
| argument of perigee: | 128.7581° |
| revolutions per day: | 14.33066884 |
| mean anomaly at epoch: | 231.4730° |
| orbit number at epoch: | 69488 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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