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 22176.56559161 .00000122 00000-0 90717-4 0 9994
2 33591 99.1469 210.8728 0014293 161.4061 198.7635 14.12580536689330
| Epoch (UTC): | 25 June 2022 13:34:27 |
| Eccentricity: | 0.0014293 |
| inclination: | 99.1469° |
| perigee height: | 840 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 210.8728° |
| argument of perigee: | 161.4061° |
| revolutions per day: | 14.12580536 |
| mean anomaly at epoch: | 198.7635° |
| orbit number at epoch: | 68933 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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