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 23342.48398496 -.00000073 00000-0 12445-3 0 9995
2 00050 47.2281 142.5780 0113853 147.7312 213.0507 12.20136206825167
| Epoch (UTC): | 08 December 2023 11:36:56 |
| Eccentricity: | 0.0113853 |
| inclination: | 47.2281° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 142.5780° |
| argument of perigee: | 147.7312° |
| revolutions per day: | 12.20136206 |
| mean anomaly at epoch: | 213.0507° |
| orbit number at epoch: | 82516 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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