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 23079.71946286 .00000354 00000-0 14536-3 0 9994
2 20442 98.8354 54.3889 0012864 79.1441 281.1189 14.33202051732671
| Epoch (UTC): | 20 March 2023 17:16:01 |
| Eccentricity: | 0.0012864 |
| inclination: | 98.8354° |
| perigee height: | 772 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 54.3889° |
| argument of perigee: | 79.1441° |
| revolutions per day: | 14.33202051 |
| mean anomaly at epoch: | 281.1189° |
| orbit number at epoch: | 73267 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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