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 23265.66935083 .00005504 00000-0 37087-3 0 9997
2 22 50.2793 251.5539 0123234 147.4389 213.4238 15.02136628403939
| Epoch (UTC): | 22 September 2023 16:03:51 |
| Eccentricity: | 0.0123234 |
| inclination: | 50.2793° |
| perigee height: | 475 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 251.5539° |
| argument of perigee: | 147.4389° |
| revolutions per day: | 15.02136628 |
| mean anomaly at epoch: | 213.4238° |
| orbit number at epoch: | 40393 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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