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 33591U 09005A 23090.84264676 .00000388 00000-0 23396-3 0 9997
2 33591 99.1100 135.5010 0014909 100.6191 259.6660 14.12722585729020
| Epoch (UTC): | 31 March 2023 20:13:24 |
| Eccentricity: | 0.0014909 |
| inclination: | 99.1100° |
| perigee height: | 839 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 135.5010° |
| argument of perigee: | 100.6191° |
| revolutions per day: | 14.12722585 |
| mean anomaly at epoch: | 259.6660° |
| orbit number at epoch: | 72902 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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