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 20624U 90046A 21110.51900303 .00000291 00000-0 17661-3 0 9995
2 20624 71.0392 157.0594 0013433 41.3933 318.8205 14.14355338595357
| Epoch (UTC): | 20 April 2021 12:27:21 |
| Eccentricity: | 0.0013433 |
| inclination: | 71.0392° |
| perigee height: | 835 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 157.0594° |
| argument of perigee: | 41.3933° |
| revolutions per day: | 14.14355338 |
| mean anomaly at epoch: | 318.8205° |
| orbit number at epoch: | 59535 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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