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 22178.92805139 .00002071 00000-0 18193-3 0 9991
2 32788 97.5337 163.8723 0013231 86.9011 273.3725 14.97562349770002
| Epoch (UTC): | 27 June 2022 22:16:23 |
| Eccentricity: | 0.0013231 |
| inclination: | 97.5337° |
| perigee height: | 565 km |
| apogee height: | 583 km |
| right ascension of ascending node: | 163.8723° |
| argument of perigee: | 86.9011° |
| revolutions per day: | 14.97562349 |
| mean anomaly at epoch: | 273.3725° |
| orbit number at epoch: | 77000 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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