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 33498U 09002G 24288.52558499 .00008746 00000-0 96512-3 0 9990
2 33498 98.1141 205.2280 0010927 29.5403 330.6428 14.87673260847407
| Epoch (UTC): | 14 October 2024 12:36:50 |
| Eccentricity: | 0.0010927 |
| inclination: | 98.1141° |
| perigee height: | 597 km |
| apogee height: | 613 km |
| right ascension of ascending node: | 205.2280° |
| argument of perigee: | 29.5403° |
| revolutions per day: | 14.87673260 |
| mean anomaly at epoch: | 330.6428° |
| orbit number at epoch: | 84740 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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