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 21263U 91032A 22145.54788977 .00000172 00000-0 89882-4 0 9997
2 21263 98.5135 146.0139 0014591 49.9837 310.2622 14.25990991613466
| Epoch (UTC): | 25 May 2022 13:08:57 |
| Eccentricity: | 0.0014591 |
| inclination: | 98.5135° |
| perigee height: | 794 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 146.0139° |
| argument of perigee: | 49.9837° |
| revolutions per day: | 14.25990991 |
| mean anomaly at epoch: | 310.2622° |
| orbit number at epoch: | 61346 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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