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 23091.19676920 .00000385 00000-0 23220-3 0 9998
2 33591 99.1099 135.8611 0014910 99.6922 260.5934 14.12722817729076
| Epoch (UTC): | 01 April 2023 04:43:20 |
| Eccentricity: | 0.0014910 |
| inclination: | 99.1099° |
| perigee height: | 839 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 135.8611° |
| argument of perigee: | 99.6922° |
| revolutions per day: | 14.12722817 |
| mean anomaly at epoch: | 260.5934° |
| orbit number at epoch: | 72907 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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