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 12168U 78026H 24357.54330514 .00000921 00000-0 64811-3 0 9992
2 12168 98.7128 191.8235 0173609 221.7240 137.0573 13.93532951225307
| Epoch (UTC): | 22 December 2024 13:02:21 |
| Eccentricity: | 0.0173609 |
| inclination: | 98.7128° |
| perigee height: | 789 km |
| apogee height: | 1043 km |
| right ascension of ascending node: | 191.8235° |
| argument of perigee: | 221.7240° |
| revolutions per day: | 13.93532951 |
| mean anomaly at epoch: | 137.0573° |
| orbit number at epoch: | 22530 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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