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 23085.94637657 .00002549 00000-0 37074-3 0 9998
2 33499 98.1828 337.1831 0009885 125.4170 234.7964 14.76785999761927
| Epoch (UTC): | 26 March 2023 22:42:46 |
| Eccentricity: | 0.0009885 |
| inclination: | 98.1828° |
| perigee height: | 632 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 337.1831° |
| argument of perigee: | 125.4170° |
| revolutions per day: | 14.76785999 |
| mean anomaly at epoch: | 234.7964° |
| orbit number at epoch: | 76192 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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