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 23335.14380516 .00003055 00000-0 43292-3 0 9999
2 33499 98.1540 229.4680 0009921 56.2101 304.0052 14.77752556799147
| Epoch (UTC): | 01 December 2023 03:27:04 |
| Eccentricity: | 0.0009921 |
| inclination: | 98.1540° |
| perigee height: | 629 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 229.4680° |
| argument of perigee: | 56.2101° |
| revolutions per day: | 14.77752556 |
| mean anomaly at epoch: | 304.0052° |
| orbit number at epoch: | 79914 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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