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 22U 59009A 23089.18065971 .00008323 00000-0 57834-3 0 9992
2 22 50.2826 7.2158 0128630 186.8802 173.0385 14.99801212377422
| Epoch (UTC): | 30 March 2023 04:20:08 |
| Eccentricity: | 0.0128630 |
| inclination: | 50.2826° |
| perigee height: | 478 km |
| apogee height: | 657 km |
| right ascension of ascending node: | 7.2158° |
| argument of perigee: | 186.8802° |
| revolutions per day: | 14.99801212 |
| mean anomaly at epoch: | 173.0385° |
| orbit number at epoch: | 37742 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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