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 22220.76422798 .00000134 00000-0 97346-4 0 9999
2 33591 99.1450 255.9917 0014554 44.6403 315.5937 14.12596459695839
| Epoch (UTC): | 08 August 2022 18:20:29 |
| Eccentricity: | 0.0014554 |
| inclination: | 99.1450° |
| perigee height: | 840 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 255.9917° |
| argument of perigee: | 44.6403° |
| revolutions per day: | 14.12596459 |
| mean anomaly at epoch: | 315.5937° |
| orbit number at epoch: | 69583 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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