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 22145.89872269 .00000141 00000-0 76966-4 0 9998
2 21263 98.5135 146.3549 0014568 49.0116 311.2322 14.25991009613514
| Epoch (UTC): | 25 May 2022 21:34:09 |
| Eccentricity: | 0.0014568 |
| inclination: | 98.5135° |
| perigee height: | 795 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 146.3549° |
| argument of perigee: | 49.0116° |
| revolutions per day: | 14.25991009 |
| mean anomaly at epoch: | 311.2322° |
| orbit number at epoch: | 61351 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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