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 33499U 09002H 23079.71279403 .00002046 00000-0 29941-3 0 9993
2 33499 98.1847 330.8647 0009505 143.4146 216.7714 14.76750350761000
| Epoch (UTC): | 20 March 2023 17:06:25 |
| Eccentricity: | 0.0009505 |
| inclination: | 98.1847° |
| perigee height: | 633 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 330.8647° |
| argument of perigee: | 143.4146° |
| revolutions per day: | 14.76750350 |
| mean anomaly at epoch: | 216.7714° |
| orbit number at epoch: | 76100 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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