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 30510U 99025AHY 22223.15570774 .00001292 00000-0 83456-3 0 9994
2 30510 99.1815 193.7474 0089356 315.4753 175.2336 14.02855174794484
| Epoch (UTC): | 11 August 2022 03:44:13 |
| Eccentricity: | 0.0089356 |
| inclination: | 99.1815° |
| perigee height: | 819 km |
| apogee height: | 949 km |
| right ascension of ascending node: | 193.7474° |
| argument of perigee: | 315.4753° |
| revolutions per day: | 14.02855174 |
| mean anomaly at epoch: | 175.2336° |
| orbit number at epoch: | 79448 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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