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 22180.46483521 .00001387 00000-0 12341-3 0 9998
2 32788 97.5336 165.3550 0013084 82.4039 277.8669 14.97567887770236
| Epoch (UTC): | 29 June 2022 11:09:21 |
| Eccentricity: | 0.0013084 |
| inclination: | 97.5336° |
| perigee height: | 565 km |
| apogee height: | 583 km |
| right ascension of ascending node: | 165.3550° |
| argument of perigee: | 82.4039° |
| revolutions per day: | 14.97567887 |
| mean anomaly at epoch: | 277.8669° |
| orbit number at epoch: | 77023 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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