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 23405U 94077B 23150.92921324 .00000000 00000-0 24713-4 0 9995
2 23405 70.9834 324.8119 0004858 267.7219 92.3347 14.15314702472788
| Epoch (UTC): | 30 May 2023 22:18:04 |
| Eccentricity: | 0.0004858 |
| inclination: | 70.9834° |
| perigee height: | 838 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 324.8119° |
| argument of perigee: | 267.7219° |
| revolutions per day: | 14.15314702 |
| mean anomaly at epoch: | 92.3347° |
| orbit number at epoch: | 47278 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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