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 22179.86348558 .00001658 00000-0 14664-3 0 9991
2 32788 97.5336 164.7747 0013147 84.2029 276.0692 14.97566043770247
| Epoch (UTC): | 28 June 2022 20:43:25 |
| Eccentricity: | 0.0013147 |
| inclination: | 97.5336° |
| perigee height: | 565 km |
| apogee height: | 583 km |
| right ascension of ascending node: | 164.7747° |
| argument of perigee: | 84.2029° |
| revolutions per day: | 14.97566043 |
| mean anomaly at epoch: | 276.0692° |
| orbit number at epoch: | 77024 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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