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 41152U 00055CK 24356.22677656 .00008433 00000-0 32882-2 0 9997
2 41152 98.8161 98.7727 0010251 329.2794 30.7787 14.29892225468838
| Epoch (UTC): | 21 December 2024 05:26:33 |
| Eccentricity: | 0.0010251 |
| inclination: | 98.8161° |
| perigee height: | 785 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 98.7727° |
| argument of perigee: | 329.2794° |
| revolutions per day: | 14.29892225 |
| mean anomaly at epoch: | 30.7787° |
| orbit number at epoch: | 46883 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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