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 23331.73918944 .00005627 00000-0 69247-3 0 9996
2 33498 98.1255 237.2475 0010081 353.9799 6.1291 14.83353151799642
| Epoch (UTC): | 27 November 2023 17:44:25 |
| Eccentricity: | 0.0010081 |
| inclination: | 98.1255° |
| perigee height: | 612 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 237.2475° |
| argument of perigee: | 353.9799° |
| revolutions per day: | 14.83353151 |
| mean anomaly at epoch: | 6.1291° |
| orbit number at epoch: | 79964 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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