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 23332.57076770 .00003120 00000-0 44221-3 0 9993
2 33499 98.1544 226.8645 0010055 63.2133 297.0104 14.77735886798332
| Epoch (UTC): | 28 November 2023 13:41:54 |
| Eccentricity: | 0.0010055 |
| inclination: | 98.1544° |
| perigee height: | 629 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 226.8645° |
| argument of perigee: | 63.2133° |
| revolutions per day: | 14.77735886 |
| mean anomaly at epoch: | 297.0104° |
| orbit number at epoch: | 79833 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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