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 32788U 08021F 22178.52715000 .00002446 00000-0 21400-3 0 9995
2 32788 97.5337 163.4856 0013271 88.1058 272.1684 14.97561916769945
| Epoch (UTC): | 27 June 2022 12:39:05 |
| Eccentricity: | 0.0013271 |
| inclination: | 97.5337° |
| perigee height: | 565 km |
| apogee height: | 583 km |
| right ascension of ascending node: | 163.4856° |
| argument of perigee: | 88.1058° |
| revolutions per day: | 14.97561916 |
| mean anomaly at epoch: | 272.1684° |
| orbit number at epoch: | 76994 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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