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 19822U 89016A 24331.07495370 .21281130 10154-5 32989-3 0 9992
2 19822 74.8618 255.1899 0030579 205.7626 338.8535 16.45288733250716
| Epoch (UTC): | 26 November 2024 01:47:56 |
| Eccentricity: | 0.0030579 |
| inclination: | 74.8618° |
| perigee height: | 132 km |
| apogee height: | 172 km |
| right ascension of ascending node: | 255.1899° |
| argument of perigee: | 205.7626° |
| revolutions per day: | 16.45288733 |
| mean anomaly at epoch: | 338.8535° |
| orbit number at epoch: | 25071 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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