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 19162U 88019D 24357.79915774 -.00000078 00000-0 93312-5 0 9994
2 19162 65.0417 196.7425 0022721 342.5140 100.9872 13.83919781849188
| Epoch (UTC): | 22 December 2024 19:10:47 |
| Eccentricity: | 0.0022721 |
| inclination: | 65.0417° |
| perigee height: | 933 km |
| apogee height: | 966 km |
| right ascension of ascending node: | 196.7425° |
| argument of perigee: | 342.5140° |
| revolutions per day: | 13.83919781 |
| mean anomaly at epoch: | 100.9872° |
| orbit number at epoch: | 84918 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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