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 23270.44125634 .00000370 00000-0 15108-3 0 9997
2 20442 98.8560 249.1990 0010739 236.3938 123.6221 14.33323139759996
| Epoch (UTC): | 27 September 2023 10:35:24 |
| Eccentricity: | 0.0010739 |
| inclination: | 98.8560° |
| perigee height: | 773 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 249.1990° |
| argument of perigee: | 236.3938° |
| revolutions per day: | 14.33323139 |
| mean anomaly at epoch: | 123.6221° |
| orbit number at epoch: | 75999 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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