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 23079.68066509 .00004281 00000-0 55398-3 0 9997
2 33498 98.1444 341.1108 0011975 80.9536 279.3030 14.81374759762302
| Epoch (UTC): | 20 March 2023 16:20:09 |
| Eccentricity: | 0.0011975 |
| inclination: | 98.1444° |
| perigee height: | 616 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 341.1108° |
| argument of perigee: | 80.9536° |
| revolutions per day: | 14.81374759 |
| mean anomaly at epoch: | 279.3030° |
| orbit number at epoch: | 76230 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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