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 00050U 60009B 23026.09265798 -.00000041 00000-0 40903-3 0 9994
2 00050 47.2330 44.5789 0114324 284.7461 74.0683 12.20126157786534
| Epoch (UTC): | 26 January 2023 02:13:25 |
| Eccentricity: | 0.0114324 |
| inclination: | 47.2330° |
| perigee height: | 1501 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 44.5789° |
| argument of perigee: | 284.7461° |
| revolutions per day: | 12.20126157 |
| mean anomaly at epoch: | 74.0683° |
| orbit number at epoch: | 78653 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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