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 32789U 08021G 22141.83905867 .00023326 00000-0 13134-2 0 9996
2 32789 97.3405 169.1091 0011974 64.7631 295.4840 15.13166117767908
| Epoch (UTC): | 21 May 2022 20:08:14 |
| Eccentricity: | 0.0011974 |
| inclination: | 97.3405° |
| perigee height: | 518 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 169.1091° |
| argument of perigee: | 64.7631° |
| revolutions per day: | 15.13166117 |
| mean anomaly at epoch: | 295.4840° |
| orbit number at epoch: | 76790 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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