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 12193U 78026AJ 24262.57647528 .00005637 00000-0 41173-2 0 9998
2 12193 98.8861 118.5231 0250917 122.6147 239.9496 13.82466465162912
| Epoch (UTC): | 18 September 2024 13:50:07 |
| Eccentricity: | 0.0250917 |
| inclination: | 98.8861° |
| perigee height: | 771 km |
| apogee height: | 1139 km |
| right ascension of ascending node: | 118.5231° |
| argument of perigee: | 122.6147° |
| revolutions per day: | 13.82466465 |
| mean anomaly at epoch: | 239.9496° |
| orbit number at epoch: | 16291 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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