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 21798U 91082A 23081.51512401 .00000165 00000-0 10436-3 0 9999
2 21798 98.8165 111.8913 0013949 63.7310 296.5296 14.16811178617872
| Epoch (UTC): | 22 March 2023 12:21:46 |
| Eccentricity: | 0.0013949 |
| inclination: | 98.8165° |
| perigee height: | 826 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 111.8913° |
| argument of perigee: | 63.7310° |
| revolutions per day: | 14.16811178 |
| mean anomaly at epoch: | 296.5296° |
| orbit number at epoch: | 61787 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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