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 32958U 08026A 22228.62609415 .00000058 00000-0 48164-4 0 9992
2 32958 98.5069 188.8129 0008145 202.4326 157.6496 14.18733231736759
| Epoch (UTC): | 16 August 2022 15:01:34 |
| Eccentricity: | 0.0008145 |
| inclination: | 98.5069° |
| perigee height: | 824 km |
| apogee height: | 835 km |
| right ascension of ascending node: | 188.8129° |
| argument of perigee: | 202.4326° |
| revolutions per day: | 14.18733231 |
| mean anomaly at epoch: | 157.6496° |
| orbit number at epoch: | 73675 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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