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 33748U 99025DJM 24356.58905846 .00003490 00000-0 13719-2 0 9994
2 33748 98.6173 45.4024 0036235 210.5488 149.3584 14.29547658863009
| Epoch (UTC): | 21 December 2024 14:08:14 |
| Eccentricity: | 0.0036235 |
| inclination: | 98.6173° |
| perigee height: | 767 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 45.4024° |
| argument of perigee: | 210.5488° |
| revolutions per day: | 14.29547658 |
| mean anomaly at epoch: | 149.3584° |
| orbit number at epoch: | 86300 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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