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 32791U 08021J 22178.63223446 .00001670 00000-0 16689-3 0 9990
2 32791 97.6113 154.6411 0013490 148.9445 211.2574 14.92716804768718
| Epoch (UTC): | 27 June 2022 15:10:25 |
| Eccentricity: | 0.0013490 |
| inclination: | 97.6113° |
| perigee height: | 580 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 154.6411° |
| argument of perigee: | 148.9445° |
| revolutions per day: | 14.92716804 |
| mean anomaly at epoch: | 211.2574° |
| orbit number at epoch: | 76871 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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