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 22177.52489532 .00002793 00000-0 24368-3 0 9993
2 32788 97.5338 162.5186 0013350 91.0131 269.2621 14.97556072769793
| Epoch (UTC): | 26 June 2022 12:35:50 |
| Eccentricity: | 0.0013350 |
| inclination: | 97.5338° |
| perigee height: | 565 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 162.5186° |
| argument of perigee: | 91.0131° |
| revolutions per day: | 14.97556072 |
| mean anomaly at epoch: | 269.2621° |
| orbit number at epoch: | 76979 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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