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 33678U 99025DFP 24356.57491224 .00004271 00000-0 94716-3 0 9990
2 33678 99.0914 31.3847 0213299 217.1602 141.4662 14.44570217908828
| Epoch (UTC): | 21 December 2024 13:47:52 |
| Eccentricity: | 0.0213299 |
| inclination: | 99.0914° |
| perigee height: | 591 km |
| apogee height: | 895 km |
| right ascension of ascending node: | 31.3847° |
| argument of perigee: | 217.1602° |
| revolutions per day: | 14.44570217 |
| mean anomaly at epoch: | 141.4662° |
| orbit number at epoch: | 90882 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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