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 23091.70328290 .00004444 00000-0 57309-3 0 9997
2 33498 98.1428 353.3260 0011609 47.0324 313.1860 14.81501778764089
| Epoch (UTC): | 01 April 2023 16:52:43 |
| Eccentricity: | 0.0011609 |
| inclination: | 98.1428° |
| perigee height: | 616 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 353.3260° |
| argument of perigee: | 47.0324° |
| revolutions per day: | 14.81501778 |
| mean anomaly at epoch: | 313.1860° |
| orbit number at epoch: | 76408 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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